IT · E-5 BIB · Entry 4 of 4 · Publication

NAVY ELECTRICITY AND ELECTRONICS TRAINING SERIES MODULE 17-RADIO-FREQUENCY COMMUNICATIONS PRINCIPLES

NAVEDTRA 14189A · CHAPTER 2, 4

Chapter 2

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2-1 UNCLASSIFIED 2 INTRODUCTION TO COMMUNICATIONS THEORY LEARNING OBJECTIVES After you finish this chapter, you should be able to do the following: 1. Describe the four basic types of transmitters. 2. Describe the two basic types of single-sideband circuits. 3. Describe the three basic types of teletypewriter circuits. 4. List the four primary functions of a basic receiver. 5. Describe the four primary functions of a basic receiver. 6. State the four characteristics of a basic receiver. 7. Evaluate the four characteristics of a basic receiver. 8. Describe the fundamental heterodyning process. 9. Describe the basic difference between an AM and an fm receiver. 10. Describe single-sideband suppressed carrier communications. 11. State the purpose of carrier reinsertion and how it is used in single-sideband communications. 12. Describe the basic theory and functions of receiver control circuits. 13. Describe the basic frequency synthesis process. 14. Describe the basic audio reproduction process.

2.1 INTRODUCTION In the previous chapter you learned the fundamentals of U.S. naval telecommunications and communications. Now, let’s look at the equipment and systems that are used to communicate in the Navy. The fundamental equipment used to communicate are the transmitter and receiver.

Transmitters and receivers must each perform two basic functions. The transmitter must generate a radio frequency signal of sufficient power at the desired frequency. It must have some means of varying (or modulating) the basic frequency so that it can carry an intelligible signal. The receiver must select the desired frequency you want to receive and reject all unwanted frequencies. In addition, receivers must be able to amplify the weak incoming signal to overcome the losses the signal suffers in its journey through space.

Representative transmitters and their fundamental features are described for you in this module.

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2-2 UNCLASSIFIED 2.2 TRANSMITTER FUNDAMENTALS Basic communication transmitters include continuous wave (cw), amplitude modulated (AM), frequency modulated (fm), and single sideband (ssb) types. A basic description of each of these transmitters is given in this chapter.

2.2.1 Continuous Wave Transmitter The continuous wave is used principally for radiotelegraphy; that is, for the transmission of short or long pulses of rf energy to form the dots and dashes of the Morse code characters. This type of transmission is sometimes referred to as interrupted continuous wave. Cw transmission was the first type of radio communication used, and it is still used extensively for long-range communications. Two of the advantages of cw transmission are a narrow bandwidth, which requires less output power, and a degree of intelligibility that is high even under severe noise conditions. (For example, when the receiver is in the vicinity of rotating machinery or thunderstorms.)

A cw transmitter requires four essential components. These are a generator, amplifier, keyer, and antenna. We have to generate rf oscillations and have a means of amplifying these oscillations. We also need a method of turning the rf output on and off (keying) in accordance with the intelligence to be transmitted and an antenna to radiate the keyed output of the transmitter.

Let’s take a look at the block diagram of a cw transmitter and its power supply in figure 2-1. The oscillator generates the rf carrier at a preset frequency and maintains it within close tolerances. The oscillator may be a self-excited type, such as an electron-coupled oscillator, or a quartz crystal type, which uses a crystal cut to vibrate at a certain frequency when electrically excited. In both types, voltage and current delivered by the oscillator are weak. The oscillator outputs must be amplified many times to be radiated any distance.

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The buffer stage or first intermediate power amplifier stage (referred to as the ipa) is a voltage amplifier that increases the amplitude of the oscillator signal to a level that drives the power amplifier (pa). You will find the signal delivered by the buffer varies with the type of transmitter and may be hundreds or thousands of volts.

The buffer serves two other purposes. One is to isolate the oscillator from the amplifier stages. Without a buffer, changes in the amplifier caused by keying or variations in source voltage would vary the load of the oscillator and cause it to change frequency. It may also be used as a frequency multiplier, which is explained later in this text.

As you can see in the figure, a key is used to turn the buffer on and off. When the key is closed, the rf carrier passes through the buffer stage; when the key is open (buffer is turned off), the rf carrier is prevented from getting through.

The final stage of a transmitter is the power amplifier (referred to as the pa). In chapter 3 of NEETS, Module 1, Matter, Energy, and Direct Current, you learned that power is the product of current and voltage (P = IE). In the power amplifier a large amount of rf current and voltage is made available for radiation by the antenna.

The power amplifier of a high-power transmitter may require far more driving power than can be supplied by an oscillator and its buffer stage. One or more low-power intermediate amplifiers are used between the buffer and the final amplifier that feeds the antenna. The main difference between many low and high-power transmitters is in the number of intermediate power-amplifier stages used.

Figure 2-1 Cw transmitter block diagram

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2-4 UNCLASSIFIED Figure 2-2 is a block diagram of the input and output powers for each stage of a typical medium power transmitter. You should be able to see that the power output of a transmitter can be increased by adding amplifier stages capable of delivering the power required. In our example, the .5 watt output of the buffer is amplified in the first intermediate amplifier by a factor of 10, (this is a times 10 [× 10] amplifier) giving us an input of 5 watts to the second intermediate amplifier. You can see in this example the second intermediate amplifier multiplies the 5 watt input to it by a factor of 5 (× 5) and gives us a 25 watt input to our power (final) amplifier. The final amplifier multiplies its input by a factor of 20 (× 20) and gives us 500 watts of power out to the antenna.

Q1. What are the four basic transmitter types? Q2. What is the function of the oscillator in a cw transmitter? Q3. What is the final stage of a transmitter?

Figure 2-2 Intermediate amplifiers increase transmitter power

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2-5 UNCLASSIFIED 2.2.2 Amplitude Modulated Transmitter In AM transmitters, the instantaneous amplitude of the rf output signal is varied in proportion to the modulating signal. The modulating signal may consist of many frequencies of various amplitudes and phases, such as the signals making up your own speech pattern.

Figure 2-3 gives you an idea of what the block diagram of a simple AM transmitter looks like. The oscillator, buffer amplifier, and power amplifier serve the same purpose as those in the cw transmitter. The microphone converts the audio frequency (af) input (a person’s voice) into corresponding electrical energy. The driver amplifies the audio, and the modulator further amplifies the audio signal to the amplitude necessary to fully modulate the carrier. The output of the modulator is applied to the power amplifier. The pa combines the rf carrier and the modulating signal in the power amplifier to produce the amplitude-modulated signal output for transmission. In the absence of a modulating signal, a continuous rf carrier is radiated by the antenna.

Figure 2-3 AM radiotelephone transmitter block diagram

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2-6 UNCLASSIFIED 2.2.3 Frequency Modulated Transmitter In frequency modulation (fm) the modulating signal combines with the carrier to cause the frequency of the resultant wave to vary with the instantaneous amplitude of the modulating signal.

Figure 2-4 shows you the block diagram of a frequency-modulated transmitter. The modulating signal applied to a varicap causes the reactance to vary. The varicap is connected across the tank circuit of the oscillator. With no modulation, the oscillator generates a steady center frequency. With modulation applied, the varicap causes the frequency of the oscillator to vary around the center frequency in accordance with the modulating signal. The oscillator output is then fed to a frequency multiplier to increase the frequency and then to a power amplifier to increase the amplitude to the desired level for transmission.

2.2.3.1 Harmonics True harmonics are always exact multiples of the basic or fundamental frequency generated by an oscillator and are created in amplifiers and their associated circuits. Even harmonics are 2, 4, 6, and so on, times the fundamental; odd harmonics are 3, 5, 7, and so on, times the fundamental. If an oscillator has a fundamental frequency of 2,500 kilohertz, the harmonically related frequencies are:

Figure 2-4 Fm transmitter block diagram

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2-7 UNCLASSIFIED 5,000………………second harmonic

7,500………………third harmonic

10,000………………fourth harmonic

12,500………………fifth harmonic

You should note that the basic frequency and the first harmonic are one and the same.

The series ascends indefinitely until the intensity is too weak to be detected. In general, the energy in frequencies above the third harmonic is too weak to be significant.

In some electronics books, and later in this chapter, you will find the term SUBHARMONIC used. It refers to a sine wave quantity (for example, an oscillator output) that has a frequency that is a submultiple of the frequency of some other sine wave quantity it helped make. For example, a wave that is half the fundamental frequency of another wave is called the second subharmonic of that wave; one with a third of the fundamental frequency is called a third subharmonic; and so forth.

Q4. What purpose does a microphone perform in an AM transmitter? Q5. In an fm transmitter, when does an oscillator generate only a steady frequency? Q6. What is a harmonic? Q7. If the fundamental frequency is 200 megahertz, what is the third harmonic?

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2-8 UNCLASSIFIED 2.2.3.2 Frequency Multiplication Designing and building a stable crystal oscillator is difficult. As operating frequencies increase, the crystal must be ground so thin that it often cracks while vibrating. You will find that you can get around this problem by operating the oscillators in most transmitters at comparatively low frequencies, sometimes as low as 1/100 (.01) of the output frequency. You raise the oscillator frequency to the required output frequency by passing it through one or more frequency multipliers. Frequency multipliers are special power amplifiers that multiply the input frequency. Stages that multiply the frequency by 2 are called doublers; those that multiply by 3 are triplers; and those multiplying by 4 are quadruplers.

You will find the main difference between low-frequency and high-frequency transmitters is the number of frequency-multiplying stages used. Figure 2-5 shows the block diagram of the frequency multiplying stages of a typical Navy uhf/vhf transmitter. The oscillator in this transmitter is tunable from 18 megahertz to 32 megahertz. You have multiplier stages that increase the oscillator frequency by a factor of 12 through successive multiplications of 2, 2, and 3.

Figure 2-6 is a block diagram of an fm transmitter showing waveforms found at various test points. In high-power applications you often find one or more intermediate amplifiers added between the second doubler and the final power amplifier.

Figure 2-5 Frequency multiplying stages of a typical vhf/uhf transmitter

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2.2.4 Single-Sideband Transmitter You should remember the properties of modulation envelopes from your study of NEETS, Module 12, Modulation Principles. A carrier that has been modulated by voice or music is accompanied by two identical sidebands, each carrying the same intelligence. In amplitude-modulated (AM) transmitters, the carrier and both sidebands are transmitted. In a single-sideband transmitter (ssb), only one of the sidebands, the upper or the lower, is transmitted while the remaining sideband and the carrier are suppressed. SUPPRESSION is the elimination of the undesired portions of the signal.

Figure 2-7 is the block diagram of a single-sideband transmitter. You can see the audio amplifier increases the amplitude of the incoming signal to a level adequate to operate the ssb generator. Usually the audio amplifier is just a voltage amplifier.

Figure 2-6 Block diagram of an fm transmitter and waveforms

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The ssb generator (modulator) combines its audio input and its carrier input to produce the two sidebands. The two sidebands are then fed to a filter that selects the desired sideband and suppresses the other one. By eliminating the carrier and one of the sidebands, intelligence is transmitted at a savings in power and frequency bandwidth.

In most cases ssb generators operate at very low frequencies when compared with the normally transmitted frequencies. For that reason, we must convert (or translate) the filter output to the desired frequency. This is the purpose of the mixer stage. A second output is obtained from the frequency generator and fed to a frequency multiplier to obtain a higher carrier frequency for the mixer stage. The output from the mixer is fed to a linear power amplifier to build up the level of the signal for transmission.

2.2.4.1 Suppressed Carrier In ssb the carrier is suppressed (or eliminated) at the transmitter, and the sideband frequencies produced by the carrier are reduced to a minimum. You will probably find this reduction (or elimination) is the most difficult aspect in the understanding of ssb. In a single-sideband suppressed carrier, no carrier is present in the transmitted signal. It is eliminated after modulation is accomplished and is reinserted at the receiver during the demodulation process. All rf energy appearing at the transmitter output is concentrated in the sideband energy as "talk power."

Figure 2-7 Ssb transmitter block diagram

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2-11 UNCLASSIFIED After the carrier is eliminated, the upper and lower sidebands remain. If one of the two sidebands is filtered out before it reaches the power amplifier stage of the transmitter, the same intelligence can be transmitted on the remaining sideband. All power is then transmitted in one sideband, instead of being divided between the carrier and both sidebands, as it is in conventional AM. This provision gives you an increase in power for the wanted sideband. You should note in figure 2-8 that the bandwidth required for the ssb suppressed carrier, view B, is approximately half that needed for conventional AM, view A. This enables us to place more signals in a smaller portion of the frequency spectrum and permits a narrower receiver bandpass.

Figure 2-8 Comparison of bandwidths of conventional AM and ssb voice channels

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2-12 UNCLASSIFIED 2.2.4.2 Applications Single-sideband transmission is the most common communications mode used today. Some of the ssb applications used in naval communications are described for you in the following paragraphs.

SSB VOICE CIRCUITS.—The high command (HICOM) network uses ssb as a means of communications between fleet commanders; and fleet commanders use it for communications between their subordinates and adjacent commands.

Ssb is generally used whenever special voice communications circuits are necessary between shore activities or between ships and shore activities because it is less susceptible to atmospheric interference than amplitude modulation.

SSB TELETYPEWRITER CIRCUITS.—With few exceptions, you will find ssb used on all longhaul (great distance) teletypewriter circuits, which includes ship-to-shore. Most of these systems are covered circuits; that is, an electronic cryptographic device on both ends of the circuit automatically encrypts and decrypts message traffic. These devices are used on point-to-point, ship-to-shore, ship-to-ship, and broadcast circuits.

Point-to-Point.—Most point -to-point, long-haul circuits between naval communications stations quickly use up the available frequency spectrum that ssb provides. Independent sideband (isb) transmission is normally used to compensate for the deficiency. Isb is used extensively in naval communications to expand our traffic capabilities. You will find there is a similarity between ssb and isb. Isb uses outputs from two sideband generators; it suppresses both carriers and then filters out an upper sideband from one and a lower sideband from the other. We then combine the two remaining sidebands and transmit an envelope with upper and lower sidebands that contain different intelligence. Isb can be used with MULTIPLEXING (a method for simultaneous transmission of two or more signals over a common carrier wave) to transmit a lot of intelligence on one circuit. Independent sideband and multiplexing will be discussed in more detail in chapter 3.

Ship-to-Shore.—Many ships handle enough message traffic to justify ship- to-shore teletypewriter circuits. Depending on traffic load, these circuits may contain from one to four (minimum) teletypewriter circuits on one sideband circuit. If the traffic load warrants more than one teletypewriter circuit, we usually use time division multiplex or frequency division multiplex (mux) equipment. This equipment is capable of handling many incoming and outgoing circuits. One circuit normally is used as an ORDERWIRE CIRCUIT for operator-to-operator service messages and for making frequency changes when necessary. The remaining circuits are available for handling official message traffic.

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2-13 UNCLASSIFIED Q8. Why are frequency multipliers used? Q9. What are two advantages of ssb transmission? Q10. What is the purpose of an order-wire circuit? Ship-to-Ship.—Ship- to-ship ssb teletypewriter circuits are in wide use today. Their main application is with task force or task group networks or with several ships in company. By using this type of network, ships can send their outgoing messages to another ship that relays traffic ashore. You can see this procedure saves manpower and circuit time, prevents individual ships from overcrowding ship-to-shore circuits, and conserves the frequency spectrum. Depending on the number and types of ships in company, the guard can be shifted to other ships from time to time. A major advantage of these circuits is that electronic cryptographic devices can be used to send classified messages without need for manual encryption. These circuits are used for incoming as well as outgoing traffic, and they can use either hf or uhf communications equipment.

2.3 RECEIVER FUNDAMENTALS An AM receiver processes amplitude-modulated signals received by its antenna. It delivers an output that is a reproduction of the signal that originally modulated the rf carrier at the transmitter. The signal can then be applied to some reproducing device, such as a loudspeaker, or to a terminal device, such as a teletypewriter. Actual AM receivers vary widely in complexity. Some are very simple; others contain a large number of complex circuits.

2.3.1 Functions Whatever its degree of sophistication, a receiver must perform certain basic functions to be useful. These functions, in order of their performance, are reception, selection, detection, and reproduction.

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2-14 UNCLASSIFIED 2.3.1.1 Reception Reception occurs when a transmitted electromagnetic wave passes through the receiver antenna and induces a voltage in the antenna.

2.3.1.2 Selection Selection is the ability of the receiver to select a particular frequency of a station from all other station frequencies appearing at the antenna of the receiver.

2.3.1.3 Detection Detection is the action of separating the low (audio) frequency intelligence from the high (radio) frequency carrier. A detector circuit is used to accomplish this action.

2.3.1.4 Reproduction Reproduction is the action of converting the electrical signals to sound waves, which can then be interpreted by your ear as speech, music, and the like. An example of this might be the stereo speakers in your car.

2.3.2 Receiver Characteristics Sensitivity, noise, selectivity, and fidelity are important receiver characteristics. These characteristics will be useful to you when performing receiver tests. They can help you to determine whether a receiver is working or not or in comparing one receiver to another.

2.3.2.1 Sensitivity The ability of a receiver to reproduce weak signals is a function of the sensitivity of a receiver. The weaker a signal that can be applied to a receiver and still produce a certain value of signal output, the better the sensitivity rating. Sensitivity of a receiver is measured under standardized conditions. It is expressed in terms of the signal voltage, usually in the microvolts that must be applied to the antenna input terminals to give an established level of the output. The output may be an ac or dc voltage measured at the detector output or a power measurement (measured in decibels or watts) at the loudspeaker or headphone terminals.

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2-15 UNCLASSIFIED 2.3.2.2 Noise All receivers generate a certain amount of noise, which you must take into account when measuring sensitivity. Receiver noise may originate from the atmosphere (lightning) or from internal components (transistors, tubes). Noise is the limiting factor of sensitivity. You will find sensitivity is the value of input carrier voltage (in microvolts) that must be applied from the signal generator to the receiver input to develop a specified output power.

2.3.2.3 Selectivity Selectivity is the degree of distinction made by the receiver between the desired signal and unwanted signals. You will find the better the ability of the receiver to reject unwanted signals, the better its selectivity. The degree of selection is determined by the sharpness of resonance to which the frequency determining circuits have been engineered and tuned. You usually measure selectivity by taking a series of sensitivity readings. As you take the readings, you step the input signal along a band of frequencies above and below the circuit resonance of the receiver; for example, 100 kilohertz below to 100 kilohertz above the tuned frequency. As you approach the tuned frequency, the input level required to maintain a given output level will fall. As you pass the tuned frequency, the required input level will rise. Input voltage levels are then compared with frequency. They can be plotted on paper or you might view them on an oscilloscope. They would appear in the form of a response curve. The steepness of the response curve at the tuned frequency indicates the selectivity of the receiver.

2.3.2.4 Fidelity The fidelity of a receiver is its ability to accurately reproduce, in its output, the signal that appears at its input. You will usually find the broader the band passed by frequency selection circuits, the greater your fidelity. You may measure fidelity by modulating an input frequency with a series of audio frequencies; you then plot the output measurements at each step against the audio input frequencies. The resulting curve will show the limits of reproduction.

You should remember that good selectivity requires that a receiver pass a narrow frequency band. Good fidelity requires that the receiver pass a broader band to amplify the outermost frequencies of the sidebands. Receivers you find in general use are a compromise between good selectivity and high fidelity.

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2-16 UNCLASSIFIED 2.3.3 Superheterodyne Receiver The superheterodyne is the type receiver most familiar to you. You probably see one daily in your home in the form of an AM and/or fm radio. We will discuss the basic workings of both AM and fm types and their differences.

2.3.3.1 Amplitude Modulation Receiver Figure 2-9 shows a block diagram with waveforms of a typical AM superheterodyne receiver developed to overcome the disadvantages of earlier type receivers. Let’s assume you are tuning the receiver. When doing this you are actually changing the frequency to which the rf amplifier is tuned. The rf carrier comes in from the antenna and is applied to the rf amplifier. The output of the amplifier is an amplified carrier and is sent to the mixer. The mixer also receives an input from the local oscillator. These two signals are beat together to obtain the IF through the process of heterodyning. (Heterodyning will be further discussed later in this chapter and was covered in NEETS, Module 12, Modulation Principles.) At this time you should note the dotted lines connecting the local oscillator, rf amplifier, and the mixer. This is used on block diagrams and schematics to indicate GANGED TUNING. Ganged tuning is the process used to tune two or more circuits with a single control. In our example, when you change the frequency of the receiver all three stages change by the same amount. There is a fixed difference in frequency between the local oscillator and the rf amplifier at all times. This difference in frequency is the IF. This fixed difference and ganged tuning ensures a constant IF over the frequency range of the receiver.

Figure 2-9 AM superheterodyne receiver and waveforms

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2-17 UNCLASSIFIED The IF carrier is applied to the IF amplifier. The amplified IF carrier is then sent to the detector. The output of the detector is the audio component of the input signal. This audio component is then passed through an audio frequency amplifier. The amplified audio component is sent to a speaker for reproduction. This allows you to hear the signal.

You should note that a superheterodyne receiver may have more than one frequency- converting stage and as many amplifiers as needed to obtain the desired power output. (Additional amplifiers are not shown.)

HETERODYNING.— As you know the intermediate frequency is developed by a process called heterodyning. This action takes place in the mixer stage (sometimes called a converter or first detector). Heterodyning is the combining of the incoming signal with the local oscillator signal. When heterodyning the incoming signal and the local oscillator signal in the mixer stage, four frequencies are produced. They are the two basic input frequencies and the sum and the difference of those two frequencies. The amplifier that follows (IF amplifier) will be tuned to the difference frequency. This difference frequency is known as the intermediate frequency (IF). A typical value of IF for an AM communications receiver is 455 kilohertz. The difference frequency is a lower frequency than either the rf input or oscillator frequencies. This lower frequency gives slightly better gain but does increase the chances of image frequency interference. Image frequencies will be discussed later in this chapter.

DETECTION.—Once the IF stages have amplified the intermediate frequency to a sufficient level, it is fed to the detector. When the mixer is referred to as the first detector, this stage would be called the second detector. The detector extracts the modulating audio signal. The detector stage consists of a rectifying device and filter, which respond only to the amplitude variations of the IF signal. This develops an output voltage varying at an audio-frequency rate. The output from the detector is further amplified in the audio amplifier and is used to drive a speaker or earphones.

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2-18 UNCLASSIFIED 2.3.3.2 Frequency Modulated Receiver The function of a frequency-modulated receiver is the same as that of an AM superheterodyne receiver. You will find some important differences in component construction and circuit design caused by differences in the modulating technique. Figure 2-10 is a block diagram showing waveforms of a typical fm superheterodyne receiver. Comparison of block diagrams in figures 2-9 and 2-10 shows that in both AM and fm receivers, the amplitude of the incoming signal is increased in the rf stages. The mixer combines the incoming rf with the local oscillator signal to produce the intermediate frequency, which is then amplified by one or more IF amplifier stages. You should note that the fm receiver has a wide-band IF amplifier. The bandwidth for any type of modulation must be wide enough to receive and pass all the side-frequency components of the modulated signal without distortion. The IF amplifier in an fm receiver must have a broader bandpass than an AM receiver.

Sidebands created by fm differ from the AM system. You should recall that the AM system consists of a single set of side frequencies for each radio-frequency signal modulated. An fm signal inherently occupies a wider bandwidth than AM because the number of extra sidebands that occur in an fm transmission is directly related to the amplitude and frequency of the audio signal.

Figure 2-10 Block diagram of an fm receiver and waveforms

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2-19 UNCLASSIFIED You should observe that only two fundamental sections of the fm receiver are electrically different from the AM receiver. These are the discriminator (detector) and the limiter.

Beyond the IF stage, the two receivers have a marked difference. AM demodulation involves the detection of variations in the amplitude of the signal; fm demodulation is the process of detecting variations in the frequency of the signal. In fm receivers a DISCRIMINATOR is a circuit designed to respond to frequency shift variations. A discriminator is preceded by a LIMITER circuit, which limits all signals to the same amplitude level to minimize noise interference. The audio frequency component is then extracted by the discriminator, amplified in the af amplifier, and used to drive the speaker.

ADVANTAGES.— In normal reception, fm signals are almost totally absent of static while AM signals are subject to cracking noises and whistles. Fm followed AM in development and has the advantage of operating at a higher frequency where a greater amount of frequencies are available. Fm signals provide much more realistic sound reproduction because of an increase in the number of sidebands. This increase in the number of sidebands allows more of the original audio signal to be transmitted and, therefore, a greater range of frequencies for you to hear.

As you can see, fm requires a wide bandpass to transmit signals. Each transmitting station must be assigned a wide band in the fm frequency spectrum. During fm transmissions, the number of significant sidebands that must be transmitted to obtain the desired fidelity is related to the deviation (change in carrier’ frequency) divided by the highest audio frequency to be used. At this point you may want to review chapter 2 of NEETS, Module 12, Modulation Principles. For example, if the deviation is 40 kilohertz and the highest audio frequency is 10 kilohertz, the modulation index is figured as shown below:

In this example, a modulation index of 4 equates to 14 significant sidebands. Because the audio frequency is 10 kilohertz and there are 14 side-bands, the bandwidth must accommodate a 140-kilohertz signal. You can see this is considerably wider than the 10- to-15-kilohertz bandpass used in AM transmitting.

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2-20 UNCLASSIFIED FREQUENCY CONVERSION.—Frequency conversion is accomplished by using the heterodyne principle of beating two frequencies together to get an intermediate frequency. So far, you have only become familiar with single conversion; however, some receivers use double or triple conversion. These methods are sometimes referred to as double or triple heterodyning. Receivers using double or triple conversion are very selective and suppress IMAGE SIGNALS to yield sharp signal discrimination. (Image signals are undesired, modulated carrier signals that differ by twice the intermediate frequency from the frequency to which the superheterodyne receiver is tuned.) Double and triple conversion receivers also have better adjacent channel selectivity than can be realized in single conversion sets.

In military communications receivers you may sacrifice fidelity to improve selectivity. This is permitted because intelligence (voice, teletypewriter) can be carried on a fairly narrow band of frequencies. Entertainment receivers, on the other hand, must reproduce a wider band of frequencies to achieve their high-fidelity objective.

Q13. What frequency conversion principle is used to develop the IF? Q14. What is the function of the detector? Q15. What is the major disadvantage of an fm signal as compared to an AM signal? 2.3.4 Single-Sideband You know from studying the single-sideband transmitter material in this chapter you may transmit only one sideband of an AM signal and retain the information transmitted. Now you will see how a single-sideband signal is received.

2.3.4.1 Advantages Figure 2-11 illustrates the transmitted signal for both AM and ssb. Ssb communications has several advantages. When you eliminate the carrier and one sideband, all of the transmitted power is concentrated in the other sideband. Also, an ssb signal occupies a smaller portion of the frequency spectrum in comparison to the AM signal. This gives us two advantages, narrower receiver bandpass and the ability to place more signals in a small portion of the frequency spectrum.

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Ssb communications systems have some drawbacks. The process of producing an ssb signal is somewhat more complicated than simple amplitude modulation, and frequency stability is much more critical in ssb communication. While we don’t have the annoyance of heterodyning from adjacent signals, a weak ssb signal is sometimes completely masked or hidden from the receiving station by a stronger signal. Also, a carrier of proper frequency and amplitude must be reinserted at the receiver because of the direct relationship between the carrier and sidebands.

Figure 2-11 Comparison of AM and ssb transmitted signals

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2-22 UNCLASSIFIED Figure 2-12 is a block diagram of a basic ssb receiver. It is not significantly different from a conventional superheterodyne AM receiver. However, a special type of detector and a carrier reinsertion oscillator must be used. The carrier reinsertion oscillator must furnish a carrier to the detector circuit. The carrier must be at a frequency which corresponds almost exactly to the position of the carrier used in producing the original signal.

Rf amplifier sections of ssb receivers serve several purposes. Ssb signals may exist in a small portion of the frequency spectrum; therefore, filters are used to supply the selectivity necessary to adequately receive only one of them. These filters help you to reject noise and other interference.

Ssb receiver oscillators must be extremely stable. In some types of ssb data transmission, a frequency stability of ±2 hertz is required. For simple voice communications, a deviation of ±50 hertz may be tolerable.

These receivers often employ additional circuits that enhance frequency stability, improve image rejection, and provide automatic gain control (agc). However, the circuits contained in this block diagram are in all single-sideband receivers.

Figure 2-12 Basic ssb receiver

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2-23 UNCLASSIFIED 2.3.4.2 Carrier Reinsertion The need for frequency stability in ssb operations is extremely critical. Even a small deviation from the correct value in local oscillator frequency will cause the IF produced by the mixer to be displaced from its correct value. In AM reception this is not too damaging, since the carrier and sidebands are all present and will all be displaced an equal amount. Therefore, the relative positions of carrier and sidebands will be retained. However, in ssb reception there is no carrier, and only one sideband is present in the incoming signal.

The carrier reinsertion oscillator frequency is set to the IF frequency that would have resulted had the carrier been present. For example, assume that a transmitter with a suppressed carrier frequency of 3 megahertz is radiating an upper sideband signal. Also assume that the intelligence consists of a 1-kilohertz tone. The transmitted sideband frequency will be 3,001 kilohertz. If the receiver has a 500-kilohertz IF, the correct local oscillator frequency is 3,500 kilohertz. The output of the mixer to the IF stages will be the difference frequency, 499 kilohertz. Therefore, the carrier reinsertion oscillator frequency will be 500 kilohertz, which will maintain the frequency relationship of the carrier to the sideband at 1 kilohertz.

Recall that 1 kilohertz is the modulating signal. If the local oscillator frequency should drift to 3,500.5 kilohertz, the IF output of the mixer will become 499.5 kilohertz. The carrier reinsertion oscillator, however, will still be operating at 500 kilohertz. This will result in an incorrect audio output of 500 hertz rather than the correct original 1-kilohertz tone. Suppose the intelligence transmitted was a complex signal, such as speech. You would then find the signal unintelligible because of the displacement of the side frequencies caused by the local oscillator deviation. The local oscillator and carrier reinsertion oscillator must be extremely stable.

Q16. What two components give a ssb receiver its advantages over an AM superheterodyne receiver?

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2-24 UNCLASSIFIED 2.3.5 Receiver Control Circuits This section deals with circuits that control receiver functions. We will explain how some of the basic manual and automatic receiver control functions work.

2.3.5.1 Manual Gain Control (mgc) You learned previously that high sensitivity is one of the desirable characteristics of a good receiver. In some cases high sensitivity may be undesirable. For example, let’s suppose the signals received from a nearby station are strong enough to overload the rf sections of your receiver. This may cause the audio output to become distorted to the point of complete loss of intelligibility. To overcome this problem, you can use manual gain control of the rf section. By using the manual gain control, you can adjust the receiver for maximum sensitivity and amplify weak input signals. When you receive a strong input signal, the rf gain may be reduced to prevent overloading. A typical manual gain control circuit for a receiver is illustrated in figure 2-13. Let’s go through the basic circuitry.

Figure 2-13 Typical rf gain control

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2-25 UNCLASSIFIED C1 is an emitter bypass capacitor. Resistors R1 and R2 develop emitter bias for the amplifier. C2 provides dc isolation between the tank and the base of transistor Q1. You should recall from your studies of NEETS, Module 7, Solid-State Devices and Power Supplies, and Module 8, Amplifiers, that amplifier gain may be varied by changing bias. Potentiometer R2, the rf gain control, is nothing more than a manual bias adjustment. When the wiper arm of R2 is set at point B, minimum forward bias is applied to the transistor. This causes the amplifier to operate closer to cutoff and reduces gain. When you move the control toward point A, the opposite occurs. R1 limits the maximum conduction of Q1 when R2 is short circuited. You may run into an alternate biasing method when the transistor is operated near saturation. In that case, a large change in gain would again be a function of bias.

2.3.5.2 Manual Volume Control (mvc) Figure 2-14 shows the circuitry for a common method of controlling volume in a superheterodyne receiver. C1 and R1 form an input signal coupling circuit and are also the means of controlling the level applied to the audio amplifier. R1, R2, and R3 develop forward bias and set the operating point for the transistor amplifier. R4 is the collector load resistor for Q1, and C3 is the output coupling capacitor. Potentiometer R1 in the circuit shown causes the input impedance of the stage to remain fairly constant. The signal from the preceding stage is felt across R1. By adjusting R1, you can change the input level to Q1 and vary the output amplitude.

Figure 2-14 Typical manual gain/volume control

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2-26 UNCLASSIFIED 2.3.5.3 Automatic Gain/Volume Control (agc/avc) Output volume variations of a receiver often result from variations in the input signal strength. Changes in input signal strength occur when we change stations or when we experience fading because of changing atmospheric conditions. The function of an AUTOMATIC GAIN CONTROL, also referred to as an AUTOMATIC VOLUME CONTROL, is to limit unwanted variations in the output of the receiver caused by variations in strength of the received signal input. A receiver without agc would require continuous manual readjustment to compensate for received signal changes so that it could maintain a constant output level.

Signals from stations operating at the same power level may not reach the receiver antenna with the same power. This is because of differences in transmission distances, carrier frequencies, atmospheric conditions, and obstructions between the transmitter and receiver antennas.

You might draw the conclusion that an agc network is not necessary when the receiver is operating on a single station. However, this is not true; atmospheric conditions may cause the signal strength to vary (fade in and out), or the antenna may receive components of the signal which have traveled along different paths. For example, one component may travel directly from the antenna, and another may have been reflected from a distant object. The two signals will sometimes be in phase and at other times be out of phase, thus tending to reinforce or cancel each other. The result is a variation in signal strength at the receiver antenna. This variation in signal strength is often referred to as FADING. The effect of fading in the output signal voltage of an rf stage is best demonstrated by the following example: An rf amplifier connected to a receiving antenna has a voltage gain of 100. If the antenna receives an input signal of 10 microvolts, the output voltage is computed as follows:

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2-27 UNCLASSIFIED With the output voltage equal to 1 millivolt, and if fading is to be avoided, the output voltage must remain at 1 millivolt. However, if a reflected signal is received that is approximately one-half the strength (5 microvolts) of the original and is in phase with the original signal, the total input signal to the receiving antenna will increase to 15 microvolts. To maintain the desired 1 millivolt of output signal, you must somehow reduce the gain of the rf amplifier. With an input of 15 microvolts and a desired output of 1 millivolt (1,000 microvolts), the gain of the amplifier must be reduced to:

When the 10-microvolt original signal and the 5-microvolt reflected signal are out of phase with each other, the signal strength at the receiving antenna will decrease to 5 microvolts. If we want to maintain our original 1,000-microvolt output signal, the voltage gain of the amplifier must be increased as follows:

A variation of amplifier gain, similar to the example, is necessary if we are going to compensate for input signal strength variations. The required amplifier gain variations can be accomplished automatically by the addition of an agc circuit within the receiver. Let’s take a look at the methods and circuits used to produce agc and the manner in which agc (avc) controls receiver gain.

CIRCUITRY.— Figure 2-15 is a block diagram representing agc feedback to preceding stages. The detector circuit has a dc component in the output that is directly proportional to the average amplitude of the modulated carrier. The agc circuitry uses this dc component by filtering the detector output to remove the audio and IF components and by applying a portion of the dc component to the preceding stages. This agc voltage controls the amplification of any or all of the stages preceding the detector stage. Solid-state receivers may use either positive or negative voltage for agc. The type of transistors used and the elements to which the control voltage is applied determine which type we will have.

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The circuit shown in figure 2-16 produces a positive agc voltage. Transformer T1, diode CR1, capacitor C1, and resistor R1 comprise a series diode detector. The agc network is made up of R2 and C2. With normal detector operation and the positive (+) potential shown at the input, CR1 conducts. Conduction of the diode will cause a charging current (shown by the dashed line) to flow through agc capacitor C2 and agc resistor R2. This charging current develops a voltage across C2. When the potential across T1 reverses, the diode will be reverse biased and will not conduct. When this happens, the charging current ceases and C2 begins to discharge. The discharge path for C2 is shown by the solid arrows. The discharge path time constant of C2, R1, and R2 is chosen to be longer than the period (1/f) of the lowest audio frequency present in the output of the detector. Because of the longer time constant, C2 will not discharge much between peaks of the modulating signal, and the voltage across C2 will be essentially a dc voltage. This voltage is proportional to the average signal amplitude. Now, if the signal strength varies, C2 will either increase or decrease its charge, depending on whether the signal increases or decreases. Since the charge on the agc capacitor responds only to changes in the average signal level, instantaneous variations in the signal will not affect the agc voltage.

Figure 2-15 Block diagram showing agc application

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You should remember that, depending on transistor types, the receiver may require either a positive or a negative agc voltage. A negative agc voltage could be easily obtained by reversing CR1. Once the values for R2 and C2 have been selected, the voltage divider action of the components is fixed, and the circuit operates automatically without further adjustment. If the average amplitude of the signal increases, the charge on C2 will also increase. If the signal amplitude decreases so does the charge on C2.

The agc voltages in a receiver provide controlled degenerative feedback. By adjusting the operating point of an amplifier, you can control the gain. Under no-signal conditions, bias of the rf and IF amplifiers is developed by standard means, such as self bias. With an applied signal, an agc voltage is developed, which in conjunction with normal biasing methods develops the operating bias for the amplifiers.

Figure 2-16 Series diode detector and simple agc circuit

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2-30 UNCLASSIFIED TRANSISTOR AMPLIFIER GAIN.—You have seen how a dc voltage that is obtained at the output of the agc network is proportional to, and will reflect, the average variations of the average signal level. Now all we have to do is use this agc voltage to control the amplification of one or more of the preceding amplifiers. Figure 2-17 illustrates a common-emitter amplifier with agc applied to the base element. A change in the agc voltage will change the operating point of the transistor and the dc emitter current. In this circuit, R1 and R4 form a voltage divider and establish no-signal (forward) bias on the base. Since a pnp transistor is used, the base has a negative potential. The agc voltage from the detector is positive with respect to ground and is fed to the base through dropping resistor R2. You will find when the dc output of the detector increases (because of an increase in the average signal level) the agc voltage will become more positive. This increased positive potential is applied to the base of Q1, which decreases the forward bias of Q1 and decreases the gain of the amplifier. Agc, in this application, works with controlled degenerative feedback. Use of an npn transistor, in the same configuration, would require the agc voltage to possess a negative potential.

FORWARD AND REVERSE AGC.—When we use an agc voltage to cause degeneration by driving the amplifiers toward cutoff, it is referred to as REVERSE agc. Figure 2-18 shows the type of agc circuitry normally used with this method. A second method that uses agc is an application called FORWARD agc. In the case of forward agc, you'll find the amplifier is driven toward the saturation region of its characteristic curve. (Sometimes referred to as an energy diagram.)

Figure 2-17 Common emitter amplifier with agc

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Let’s look at our example. Assume the agc voltage is negative. Under this condition, Q1 is self biased; under no-signal conditions, it is operating well up on its characteristic curve. When a signal is applied, negative agc voltage is developed in the detector circuit and fed back to Q1, which increases forward bias. Any increase in signal level causes an increase in agc voltage. An increase in agc voltage increases conduction, which in turn drives the transistor to or near saturation. As the transistor approaches saturation, its gain is correspondingly reduced.

On the other hand, if the input signal level decreases, the negative agc voltage decreases. The forward bias is then reduced, and the transistor operates on a lower portion of its characteristic curve where gain is higher.

Forward agc provides you with better signal-handling capabilities; however, reverse agc is simpler to use, causes less loading of the tuned circuits, and produces smaller variations in input and output capacitance.

Figure 2-18 Reverse agc

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2-32 UNCLASSIFIED Q17. What does manual gain control do to strong and weak signals, respectively? Q18. What is the purpose of agc/avc in a receiver? 2.3.5.4 Delayed Automatic Gain Control The disadvantage of automatic gain control, attenuating even the weak signal, is overcome by the use of delayed automatic gain control (dagc). Let’s take a look at the typical dagc circuitry in figure 2-19. This type of system develops no agc feedback until an established received signal strength is attained. For signals weaker than this value, no agc is developed. For sufficiently strong signals, the delayed agc circuit operates essentially the same as ordinary agc.

Figure 2-19 Delayed agc action

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2-33 UNCLASSIFIED Our circuit uses two separate diodes; one is the detector diode and the other the agc diode. The agc diode is connected to the primary of the last IF transformer and the detector diode to its secondary. A positive bias is applied to the cathode of the agc diode. This keeps it from conducting until a prearranged signal level has been reached. The adjust delay control allows manual control of the agc diode bias. Manual control allows you to select the signal level at which agc is applied. If mostly weak stations are to be received, the setting should be high (no agc until the signal level is high). However, you should set it as low as possible to prevent overloading of the last IF amplifier by stronger signals.

Finally, you must have two diodes to obtain delayed agc. If only one diode were used, the agc would be developed from the detector diode, and there would be no delayed action. Or, if a signal diode were biased to provide the delaying action desired, no signal would pass to the audio amplifier until the bias was exceeded by the input signal.

2.3.5.5 Beat-Frequency Oscillator The beat-frequency oscillator (bfo) is necessary when you want to receive cw signals. Cw signals are not modulated with an audio component, you remember, so we must provide one. The action of the rf amplifier, mixer, local oscillator, and IF amplifier is the same for both cw and AM; but the cw signal reaches the detector as a single frequency signal with no sideband components. To produce an af output, you must heterodyne (beat) any cw signal with an rf signal of the proper frequency. This separate signal is obtained from an oscillator known as a beat-frequency oscillator.

Figure 2-20 is a block diagram of a superheterodyne receiver capable of receiving and demodulating a cw signal. The bfo heterodynes at the detector and produces an af output. The detector (second detector) is used primarily because the mixer (first detector) is normally used as the source of agc.

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If the intermediate frequency is 455 kilohertz and the bfo is tuned to 456 kilohertz or 454 kilohertz, the difference frequency of 1 kilohertz is heard in the output. Generally, you will tune the bfo from the front panel of a receiver. When you vary the bfo control, you are varying the output frequency of the bfo and will hear changes in the tone of the output audio signal.

2.3.5.6 Squelch The sensitivity of a receiver is maximum when no signal is being received. This condition occurs, for example, when a receiver is being tuned between stations. At this time background noise is picked up by the antenna, and you will hear noise greatly amplified. This noise is highly annoying and occurs because receiver gain is maximum without a signal. You can often overcome this problem by using a circuit called a SQUELCH, NOISE SILENCER, NOISE SUPPRESSOR, or NOISE LIMITER. All of these noise type circuits just clip the peaks of the noise spikes. Squelch will actually eliminate noise. Figure 2-21 is a typical circuit of this type. The circuit cuts off receiver output when no input signal is being received. It accomplishes this by blocking either the detector or audio amplifier when no signal is present. Let’s take a look at the theory involved in this process.

Figure 2-20 Placement of the beat frequency oscillator

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The squelch diode CR1 connects the output of the first af stage to the input of the second. Amplifier Q1 serves as the control transistor for the circuit. The anode and cathode voltages of CR1 are normally biased positive with respect to ground.

With no input signal, R9 is adjusted until Q1 draws enough collector current to reduce its collector voltage and the anode voltage of CR1 to a value below the voltage on the cathode of CR1. At this point the anode voltage of the squelch diode is negative with respect to its cathode, and conduction ceases. Audio output is now reduced to zero and the receiver is silent.

The base of Q1 is connected to the automatic volume control (avc) line. Anytime a signal enters the receiver, a negative avc voltage is applied to the base of Q1. This reduces the collector current and increases the collector voltage, which in turn increases the anode voltage of CR1 until the anode becomes positive with respect to the cathode. Once again diode CR1 will conduct, and the signal will be passed to the second af amplifier. Diode CR1 is effectively a switch controlled by the avc voltage.

Q19. What is a disadvantage of agc? Q20. What is the main difference between agc and dagc?

Figure 2-21 Squelch circuit

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2-36 UNCLASSIFIED Q21. What is the function of the bfo? Q22. What is the purpose of a squelch circuit? 2.3.5.7 Audio Tone The tone of the sound reproduced in the audio section of a receiver depends on several factors. The frequency response of the audio amplifiers determines the degree of amplification provided to different frequencies in the sound spectrum. The size and quality of any loudspeaker used will determine its response to various frequencies. Response of the human ear is the final judge of tonal quality, and that varies with the individual.

Because of these variables, some form of tone control is sometimes used in Navy receivers. Treble tones are defined as the audio frequencies above approximately 3,000 hertz and bass tones are those below approximately 300 hertz. Although several methods of tone control can be used, we are only going to mention the attenuation method. With this method, a decrease in the intensity of one tone can produce an apparent increase in the intensity of another tone. As an example, let’s look at tones of 400 and 4,000 hertz produced by a speaker with the same intensity. If we reduce the intensity of the 4,000- hertz tone, the 400-hertz tone will appear to be louder, even though its intensity has not actually changed. You should see from this example that bass emphasis can be accomplished by attenuating treble tones.

The simplest type of tone control is illustrated in figure 2-22. Fixed capacitor C1 parallels the primary winding of the output transformer, effectively shunting the higher frequencies to ground. The size of C1 determines the lowest frequency to be affected. When you select the BASS position of the tone control, C1 is connected and improves bass response by de-emphasizing the treble tones. You can often use this circuit to improve the output of a small speaker with poor treble response.

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A continuously variable tone control is illustrated in figure 2-23. Tone control R1 and bypass capacitor C1 act as a variable RC filter. With the wiper arm of R1 in the upper (BASS) position, C1 bypasses the higher frequencies to ground and provides better bass response. When the wiper arm of R1 is in the lower (TREBLE) position, the resistance of R1 is placed in series with C1, which reduces the shunting effect of C1 to high frequencies and improves the treble response. This method gives you the advantage of smooth, continuous tone control at all points between maximum bass and maximum treble response.

Figure 2-22 Fixed capacitor tone control Figure 2-23 Variable tone control using an RC filter

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2-38 UNCLASSIFIED A switch-type, variable tone control is illustrated in figure 2-24. With this method we use a three position switch to provide fixed degrees of tone control. When tone control S1 is in the BASS position, capacitor C1 bypasses the high frequencies and provides bass emphasis. With S1 in the normal (NORM) position, C2 acts as the bypass, and a moderate amount of high-frequency attenuation is accomplished. This position provides balanced bass and treble response. When S1 is in the TREBLE position, C3 acts as the bypass and provides minimum high-frequency attenuation and maximum treble emphasis. As a rule of thumb, you can figure the capacitance of C2 is approximately five times the value of C3, and C1 is approximately ten times the value of C3. For example with C3 at .001 microfarads, C2 would be .005 microfarads, and C1 would be .01 microfarads.

2.3.5.8 Crystal Filters A quartz crystal, used as a selective filter in the IF section of a communications receiver, is one of the most effective methods of achieving maximum selectivity. It is especially useful when the channel is crowded and considerable noise (both external and internal) is present.

One possible circuit arrangement is shown in figure 2-25. Let’s look at the theory involved in understanding this circuit. You can see a crystal in one leg of the bridge circuit. The secondary of the input transformer (T1) is balanced to ground through the center tap connection. The crystal acts as a high Q series resonant circuit. It allows signals within the immediate vicinity of resonance to pass through the crystal to the output coil (L3). The desired signal appears between the center tap of L3 and ground.

Figure 2-24 Switch tone control

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The capacitance that exists between the crystal holder plates (C3) may bypass unwanted signals around the crystal; therefore, some method must be provided to balance out this capacitance. You accomplish circuit balancing by applying out-of-phase voltages to neutralize any undesired signal voltages. The tap on L3 permits proper impedance matching and is the balanced input to the next stage.

Q23. What does a tone control circuit in a receiver do to the audio signal? Q24. What is the function of a crystal filter in a receiver? 2.3.5.9 Automatic Frequency Control Afc circuits are used in situations where you must accurately control the frequency of an oscillator by some external signal. Basically, this type circuit does two things: It senses the difference between the actual oscillator frequency and the frequency that is desired and produces a control voltage proportional to the difference; it also uses the control voltage to change the oscillator to the desired frequency. Afc circuits are used to control the frequency of sinusoidal oscillators and nonsinusoidal oscillators. Only sinusoidal afc circuits will be covered here. Afc circuits are used in radio receivers, fm transmitters, and frequency synthesizers to maintain frequency stability. Figure 2-26 is a block diagram illustrating afc operation in a receiver. Let’s run through the applicable parts of this block diagram.

Figure 2-25 Crystal filter used in the IF section of a superheterodyne receiver

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The frequency discriminator controls the varicap in this receiver. A varicap is used to keep the IF stable. You may want to review varicap theory in chapter 3 of NEETS, Module 7, Solid-State Devices and Power Supplies at this point. The varicap application here produces an apparent reactance, which is included in the oscillator frequency control circuitry. For example, let’s assume the IF is 455 kilohertz and the local oscillator (lo) is tracking below the incoming station. When the lo output decreases slightly in frequency, the IF will rise. This causes the output of the discriminator to increase the capacitive reactance of the varicap, which increases the oscillator frequency to the desired value. Now let’s assume the lo output increases. The IF will then decrease. This causes the discriminator output to decrease the capacitive reactance of the varicap. This will cause the oscillator frequency to decrease.

Figure 2-27 shows another widely used type of afc and its circuitry. This type is commonly referred to as a BALANCED-PHASE DETECTOR or PHASE- DISCRIMINATOR. This circuit uses fixed capacitors and the varying conductance of the diodes to achieve a variable reactance. As you have seen in the block diagram, an afc circuit requires two sections, a frequency detector and a variable reactance. Our detector output is a dc control voltage proportional to the amount of frequency change. This dc voltage is applied directly to the oscillator. The phase inverter input signals are discriminated IF outputs fed to the two diodes 180 degrees out of phase.

Figure 2-26 Block diagram of receiver showing automatic frequency control

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A reference voltage is also applied to both diodes. The diodes are biased to conduct only during the peak portions of the input signals. Any change in oscillator frequency will alter the phase relationship between the sawtooth reference voltage and the incoming signals. If this happens, one diode will conduct more than the other and produce a control signal. This system remains unbalanced at all times because any change in frequency is instantaneously corrected. The network between the diodes and oscillator is essentially a low-pass filter. This filter prevents discriminator pulses from reaching the oscillator.

2.4 FREQUENCY SYNTHESIS In present day communications systems, long term accuracy of one part in a million is required from many of the frequency generators (local oscillators) used in communications equipment. Variable frequency oscillators cannot practically achieve this high degree of stability. Therefore, a system known as FREQUENCY SYNTHESIS has been developed to meet the stringent demands for stability. This system uses circuitry that produces a signal frequency through a heterodyning and frequency selection process. This signal is not harmonically related to any of the signals used in the heterodyning process. It is also not related to the selected crystal frequency. This makes the signal unique.

Figure 2-27 Automatic frequency control (phase discriminator)

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2-42 UNCLASSIFIED Figure 2-28 is a multiple crystal, frequency synthesizer that produces desired output frequencies by mixing frequencies from several crystal oscillators. Each oscillator uses ten or more crystals to control its operating frequency. This provides for a large number of output frequency combinations. Figure 2-29 is a practical frequency synthesizer in which the harmonics and subharmonics of a single standard oscillator are combined to provide a wide multichoice of output signals. Each of these signals is harmonically related to a subharmonic of the standard oscillator. You will find the primary difficulty encountered in the frequency synthesizers is the presence of spurious signals generated in the "combining mixers." Extensive filtering and extremely careful selection of operating frequencies are required for even the simplest circuits. Spurious frequency problems increase and channel spacing decreases as the range of operating frequencies increases.

Figure 2-28 Multiple crystal frequency synthesizer Figure 2-29 Simple crystal frequency synthesizer

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2-43 UNCLASSIFIED Q25. What is the primary function of an afc circuit? Q26. What is frequency synthesis? 2.5 AUDIO REPRODUCTION DEVICES The purpose of audio reproduction devices, such as loudspeakers and headphones, is to convert electrical audio signals to sound power. Figure 2-30 shows you a diagram of a loudspeaker called the PERMANENT MAGNET SPEAKER. This speaker consists of a permanent magnet mounted on soft iron pole pieces, a voice coil that acts as an electromagnet, and a loudspeaker cone connected to the voice coil. The audio signal has been previously amplified (in terms of both voltage and power) and is applied to the voice coil. The voice coil is mounted on the center portion of the soft iron pole pieces in an air gap so that it is mechanically free to move. It is also connected to the loudspeaker cone; as it moves, the cone will also move. When audio currents flow through the voice coil, the coil moves back and forth proportionally to the applied ac current. As the cone (diaphragm) is attached to the voice coil, it also moves in accordance with the signal currents; in so doing, it periodically compresses and rarefies the air, which produces sound waves.

Figure 2-30 Permanent magnet speaker

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2-44 UNCLASSIFIED Most speakers of the above type receive their input by means of transformer coupling. This is necessary because of the normal, low impedance of the voice coil. You will find the standard impedance values for this type speaker are 4, 8, 16, and 32 ohms. Other impedance values may be obtained, but those listed are the most common.

While permanent magnet speakers perform reasonably well in the audio range, they have limitations. Most Navy speakers reproduce low audio frequencies quite well, mid-band frequencies fairly well, and high frequencies quite poorly. Let’s see why. When the speaker is constructed, only a limited number of turns may be built into the voice coil. This gives us a fixed inductance. At low frequencies, the inductive reactance of the voice coil is relatively low, and large audio currents flow. This provides a strong magnetic field around the voice coil and a strong interaction with the field of the permanent magnet. Low frequency response is excellent. At midband frequencies, inductive reactance increases and less current flows in the voice coil. This produces less magnetic field and less interaction. Midband response is still acceptable in a properly designed speaker. At high audio frequencies inductive reactance is quite high, and little current flows in the voice coil. This results in a greatly reduced voice coil field and little interaction with the permanent magnetic field. Also at high frequencies the interwinding capacitance of the voice coil tends to shunt some of the high audio frequencies, which further reduces the high frequency response.

Frequency response of most permanent magnet speakers falls off at the higher audio frequencies. This problem is normally overcome either by the use of an expensive, specially designed speaker, or through the use of two speakers, one of which is designed to operate well at the higher audio frequencies (tweeter) and one at the lower frequencies (woofer).

As shown in figure 2-31, an electromagnet may be used in place of a permanent magnet to form an electromagnetic dynamic speaker. When we do this, sufficient dc power must be available to energize the field electromagnet. The operation otherwise is much the same as that of the permanent magnet type. This type of speaker is seldom used in Navy equipment.

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Figure 2-32 shows a diagram of typical headphones used with Navy equipment. The device consists of a permanent magnet and two small electromagnets through which the signal currents pass. A soft iron diaphragm is used to convert the electrical effects of the device into sound power. When no signal currents are present, the permanent magnet exerts a steady pull on the soft iron diaphragm. Signal current flowing through the coils mounted on the soft iron pole pieces develops a magnetomotive force that either adds to or subtracts from the field of the permanent magnet. The diaphragm thus moves in or out according to the resultant field. Sound waves are then reproduced that have an amplitude and frequency (within the mechanical capability of the reproducer) similar to the amplitude and frequency of the signal currents.

Figure 2-31 Electromagnetic speaker

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As compared to permanent magnet speakers, standard headphones are considered to be high impedance devices. Headphone electromagnets are normally wound with many turns of small wire, which provide the larger impedance. Because of the physically small size and inflexibility of the metal diaphragm, the headphones often give poor response to the lower audio frequencies. In the voice range of audio, most standard issue headphones are adequate.

2.6 SUMMARY In this chapter you learned transmitter and receiver fundamentals. We also discussed modes of operation and special controls circuits. Let’s review some of these areas.

A HARMONIC is an exact multiple of the fundamental frequency. Even harmonics are 2, 4, and so on, times the fundamental. Odd are 3, 5, and so on, times the fundamental frequency.

A SUBHARMONIC is an exact submultiple of the fundamental frequency. Even subharmonics are one-half, one-quarter, and so on. Odd subharmonics are one-third, one- fifth, and so on, of the fundamental frequency.

Figure 2-32 Headphone

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2-47 UNCLASSIFIED SUPPRESSION is the process of eliminating an undesired portion of a signal.

MULTIPLEXING is a method for simultaneous transmission of two or more signals over a common carrier wave.

An ORDER-WIRE CIRCUIT is a circuit between operators used for operations control and coordination.

RECEPTION is when an electromagnetic wave passes through a receiver antenna and induces a voltage in that antenna.

DETECTION is the separation of low-frequency (audio) intelligence from the high (radio) frequency carrier.

REPRODUCTION is the process of converting electrical signals to sound waves. This sound is speech, music, and so on.

SENSITIVITY of a receiver is the ability to reproduce weak signals. The greater the receiver sensitivity, the weaker the signal that will be reproduced.

Receiver SELECTIVITY is the ability to select the desired signal and reject unwanted signals.

NOISE SILENCER, NOISE SUPPRESSOR, or NOISE LIMITER, are circuits that clip the peaks of the noise spikes in a receiver.

SQUELCH is a circuit that cuts off the output of a receiver when there is no input.

A BALANCED-PHASE DETECTOR or PHASE-DISCRIMINATOR is a circuit that controls the oscillator frequency (afc).

FREQUENCY SYNTHESIS is a signal-producing process through heterodyning and frequency selection.

A PERMANENT MAGNET SPEAKER is one with a permanent magnet mounted on soft iron pole pieces.

The FIDELITY of a receiver is the ability to accurately reproduce at its output the signal at its input.

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2-48 UNCLASSIFIED GANGED TUNING is the process used to tune two or more circuits with a single control.

HETERODYNING is the mixing of the incoming signal with the local oscillator frequency. This produces the two fundamentals and the sum and difference frequencies.

An IMAGE FREQUENCY is an undesired frequency capable of producing the desired frequency through heterodyning.

AUTOMATIC VOLUME/GAIN CONTROL is a circuit used to limit variations in the output signal strength of a receiver.

FADING is the variations in signal strength at the antenna of a receiver.

REVERSE AGC is when an amplifier is driven toward cutoff.

FORWARD AGC is when an amplifier is driven toward saturation.

A BEAT-FREQUENCY OSCILLATOR is an additional oscillator used in a receiver when the receiver is receiving a cw signal and provides an audible tone.

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2-49 UNCLASSIFIED ANSWERS TO QUESTIONS Q1. THROUGH Q26. A1. Am, fm, cw, ssb.

A2. It generates an rf carrier at a given frequency within required limits.

A3. Power amplifier.

A4. It converts audio (sound) into electrical energy.

A5. When no modulation is present.

A6. It is an exact multiple of the basic or fundamental frequency.

A7. 600 megahertz.

A8. To obtain higher carrier frequencies.

A9. It saves power and frequency bandwidth.

A10. For operator-to-operator service messages and frequency changes.

A11. Reception, selection, detection, and reproduction.

A12. Sensitivity, noise, selectivity, and fidelity.

A13. Heterodyning.

A14. To extract the modulating audio signal.

A15. Wide bandpass.

A16. A special type of detector and a carrier reinsertion oscillator.

A17. Attenuates the strong and amplifies the weak.

A18. To limit unwanted variations in the output.

A19. Weak signals produce bias, which could result in no usable receiver output.

A20. Dagc does not attenuate weak signals.

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2-50 UNCLASSIFIED A21. It is heterodyned with the rf to produce an audio frequency.

A22. It eliminates noise when no signal is being received.

A23. It controls the amount of bass and treble response.

A24. It is used to achieve maximum selectivity.

A25. It is used to accurately control the frequency of the oscillator.

A26. The process of selecting and/or heterodyning frequencies to produce a signal frequency.

Chapter 4

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4-1 UNCLASSIFIED 4 INTRODUCTION TO SATELLITE COMMUNICATIONS LEARNING OBJECTIVES After you finish this chapter, you should be able to do the following: 1. Describe the basic operation of the two types of satellites. 2. Describe the basic components of an operational satellite system. 3. Describe the function of earth terminal equipment. 4. Describe the basic signal flow of a typical shipboard receive-only system. 5. Describe the basic signal flow of a typical shipboard transceiver system. 6. Describe the advantages of satellite communications in terms of capacity, reliability, vulnerability, and flexibility. 7. Describe the limitations of satellites in terms of power, receiver sensitivity, and availability.

4.1 HISTORY OF SATELLITE COMMUNICATIONS The first artificial satellite was placed in orbit by the Russians in 1957. That satellite, called Sputnik, signaled the beginning of an era.

The United States, who was behind the Russians, made an all-out effort to catch up, and launched Score in 1958. That was the first satellite with the primary purpose of communications.

The first regular satellite communications service was used by the Navy in 1960. The moon was used to bounce teletypewriter signals between Hawaii and Washington, D.C. During the early 1960s, the Navy used the moon as a medium for passing messages between ships at sea and shore stations. This method of communications proved reliable when other methods failed.

Military satellite communications technology was at a low level until 1965. At that time high quality voice transmissions were conducted between a satellite and two earth stations. That was the stepping stone to the Initial Defense Communications Satellite Program (IDCSP), which will be covered later in this chapter.

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4-2 UNCLASSIFIED Experience with satellite communications has demonstrated that satellite systems can satisfy many military requirements. They are reliable, survivable, secure, and a cost effective method of telecommunications. You can easily see that satellites are the ideal, if not often the only, solution to problems of communicating with highly mobile forces. Satellites, if properly used, provide much needed options to large, fixed-ground installations.

For the past fifty years, the Navy has used high-frequency (hf) transmissions as the principal method of sending messages. In the 1970s, the hf spectrum was overcrowded and "free" frequencies were at a premium. Hf jamming and electronic countermeasures (ECM) techniques became highly sophisticated during that period. As a result the need for new and advanced long-range transmission methods became apparent.

Communications via satellite is a natural outgrowth of modern technology and of the continuing demand for greater capacity and higher quality in communications.

In the past, the various military branches have had the resources to support their communications needs. Predicted usage indicates that large-scale improvements will have to be made to satisfy future needs of the Department of Defense. These needs will require greater capacity for long-haul communications to previously inaccessible areas. Satellite communications has the most promise for satisfying these future requirements.

4.2 DEFENSE COMMUNICATIONS SATELLITE PROGRAM (DCSP) The Defense Communications Satellite Program (DCSP) was initiated by the Secretary of Defense in 1962. Phase I of the program was given the title Initial Defense Communications Satellite Program (IDCSP). The first satellite launch occurred in June 1966 when seven experimental satellites were placed into orbit. The final launch of this program consisted of eight satellites and occurred in June 1968.

4.3 DEFENSE SATELLITE COMMUNICATIONS SYSTEM (DSCS) PHASE II The Phase II Defense Satellite Communications System (DSCP Phase II) has changed from an all analog communications system to an all-digital communications system. The performance capability provided by the Phase II DSCS is limited by equipment availability. Extensive digital traffic capability has become common. You can credit this to the availability of digital modems (modulator/demodulator) and broadband equipment. Overall performance of the Phase II DSCS is a great improvement over the capabilities provided by Phase I DSCS. The Phase II satellites provide a great increase in effective radiated power and rf bandwidths. You will find these satellite configurations use wide coverage and narrow beam antennas. They provide an extensive range of communications services and capabilities. (This will be further discussed later, in this chapter.)

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4-3 UNCLASSIFIED 4.4 FUNDAMENTAL SATELLITE COMMUNICATIONS SYSTEM A satellite communications system uses satellites to relay radio transmissions between earth terminals. The two types of communications satellites you will study are ACTIVE and PASSIVE. A passive satellite only reflects received radio signals back to earth. An active satellite acts as a REPEATER; it amplifies signals received and then retransmits them back to earth. This increases signal strength at the receiving terminal to a higher level than would be available from a passive satellite.

A typical operational link involves an active satellite and two or more earth terminals. One station transmits to the satellite on a frequency called the UP-LINK frequency. The satellite then amplifies the signal, converts it to the DOWN-LINK frequency, and transmits it back to earth. The signal is next picked up by the receiving terminal. Figure 4-1 shows a satellite handling several combinations of links simultaneously.

Figure 4-1 Satellite communications system

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4-4 UNCLASSIFIED 4.5 DESCRIPTION OF COMMUNICATIONS SATELLITE SYSTEM The basic design of a satellite communications system depends to a great degree upon the characteristics of the orbit of the satellite. In general terms, an orbit is either elliptical or circular in shape. A special type of orbit is a SYNCHRONOUS ORBIT. In this type you will find the period (time required for one revolution) of the orbit the same as that of the earth. An orbit that is not synchronous is called ASYNCHRONOUS. A period of orbit that approaches that of the earth is called NEAR SYNCHRONOUS (subsynchronous). Orbits are discussed in more detail later in this chapter.

In addition to the fundamental components shown in figure 4-1, the design of the overall system determines the complexity of the various components and the manner in which the system operates. Current satellites are capable of handling many teletypewriter (tty) and voice circuits at the same time.

4.5.1 Orbit Descriptions Orbits generally are described according to the physical shape of the orbit and the angle of inclination of the plane of the orbit. These terms aye discussed in the following paragraphs:

PHYSICAL SHAPE.— All satellites orbit the earth in elliptical orbits. (A circle is a special case of an ellipse.) The shape of the orbit is determined by the initial launch parameters and the later deployment techniques used.

PERIGEE and APOGEE are two, of the three parameters used to describe orbital data of a satellite. These are shown on figure 4-2. Perigee is the point in the orbit nearest to the center of the earth. Apogee is the point in the orbit the greatest distance from the center of the earth. Both distances are expressed in nautical miles.

Figure 4-2 Elliptical satellite orbit

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4-5 UNCLASSIFIED ANGLE OF INCLINATION.—The ANGLE OF INCLINATION (angle between the equatorial plane of the earth and the orbital plane of the satellite) is the third parameter used to describe the orbit data of a satellite. Figure 4-3 depicts the angle of inclination between the equatorial plane and the orbital plane. Most satellites orbit the earth in orbital planes that do not coincide with the equatorial plane of the earth. A satellite orbiting in any plane not identical with the equatorial plane is in an INCLINED ORBIT.

The inclination of the orbit determines the area covered by the path of the satellite. As shown in figure 4-4, the greater the inclination, the greater the amount of surface area covered by the satellite.

Figure 4-3 Inclined satellite orbit

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4-6 UNCLASSIFIED

SPECIAL TYPES OF INCLINED ORBITS.—A satellite orbiting in a plane that coincides with the equatorial plane of the earth is in an EQUATORIAL ORBIT. A satellite orbiting in an inclined orbit with an angle of inclination of 90 degrees or near 90 degrees is in a POLAR ORBIT.

SPECIAL TYPES OF CIRCULAR ORBITS.—We stated previously that a circular orbit is a special type of elliptical orbit. You should realize a circular orbit is one in which the major and minor axis distances are equal or approximately equal. Mean height above earth, instead of perigee and apogee, is used in describing a circular orbit. While we are discussing circular orbits, you should look at some of the terms mentioned earlier in this chapter. A satellite in a circular orbit at a height of approximately 19,300 nautical miles above the earth is in a synchronous orbit. At this altitude the period of rotation of the satellite is 24 hours, the same as the rotation period of the earth. In other words, the orbit of the satellite is in sync with the rotational motion of the earth. Although inclined and polar synchronous orbits are possible, the term synchronous usually refers to a synchronous equatorial orbit. In this type of orbit, satellites appear to hover motionlessly in the sky. Figure 4-5 shows how one of these satellites can provide coverage to almost half the surface of the earth.

Figure 4-4 Effect of orbit plane inclination on satellite coverage

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4-7 UNCLASSIFIED

Three of these satellites can provide coverage over most of the earth (except for the extreme north and south polar regions). A polar projection of the global coverage of a three-satellite system is shown in figure 4-6.

Figure 4-5 Illumination from a synchronous satellite Figure 4-6 Worldwide synchronous satellite system viewed from above the North Pole

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4-8 UNCLASSIFIED A satellite in a circular orbit at other than 19,300 nautical miles above the earth is in a near synchronous orbit. If the orbit is lower than 19,300 nautical miles, the period of orbit of the satellite is less than the period of orbit of the earth. The satellite then appears to be moving slowly around the earth from west to east. (This type of orbit is also called subsynchronous.) If the orbit is higher than 19,300 nautical miles, the period of orbit of the satellite is greater than the period of orbit of the earth. The satellite then appears to be moving slowly around the earth from east to west. Although inclined and polar near- synchronous orbits are possible, near synchronous implies an equatorial orbit.

A satellite in a circular orbit from approximately 2,000 miles to 12,000 miles above the earth is considered to be in a MEDIUM ALTITUDE ORBIT. The period of a medium altitude satellite is considerably less than that of the earth. When you look at this altitude satellite, it appears to move rather quickly across the sky from west to east.

Q1. What are the two types of communications satellites? Q2. A typical satellite communications operational link consists of a satellite and what two other components? Q3. A satellite in a synchronous orbit can cover how much of the surface of the earth? Q4. What areas of the earth are not normally covered by satellites?

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4-9 UNCLASSIFIED 4.6 SATELLITE CHARACTERISTICS As early as June 1960, two satellites were successfully placed in orbit by the same launch vehicle. With the development of multilaunch capability, added flexibility became available. We then had choices as to the size, weight, and number of satellites to be included in each launch.

Using our multi-launch capabilities, the Defense Satellite Communications System (DSCS) has placed larger and heavier satellites in synchronous equatorial orbits. Figure 4-7 is a drawing of a DSCS satellite. It shows each pair of transmit and receive dish antennas. As you can see, a large area of the earth can be covered using only one satellite.

4.6.1 Satellite Power Sources Early communications satellites were severely limited by the lack of suitable power sources. This severely limited the output power of the satellite transmitter. The only source of power available within early weight restrictions was a very inefficient panel of solar cells without battery backup. A major disadvantage of this type of power source is that the satellite has no power when it is in ECLIPSE (not in view of the sun). For continuous communications, this outage is unacceptable.

Figure 4-7 DSCS satellite

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4-10 UNCLASSIFIED A combination of solar cells and storage batteries is a better prime power source. This is a practical choice, even though the result is far from an ideal power source. About ten percent of the energy of the sunlight that strikes the solar cells is converted to electrical power. This low rate is sometimes decreased even further. You find this when the solar cells are bombarded by high-energy particles that are sometimes found in space.

Early satellites had over 8,500 solar cells mounted on the surface of the satellite, which supplied about 42 watts of power. No battery backup was provided in these satellites.

Newer communications satellites have about 32,000 solar cells mounted on the surface of the satellite, and they supply about 520 watts. A nickel cadmium battery is used for backup power during eclipses.

Nuclear power sources have been used in space for special purposes, but their use stops there. Technology has not progressed sufficiently for nuclear power sources to be used as a power source.

4.6.2 Satellite Orientation Satellite orientation in space is important for continuous solar cell and antenna orientation. Since the primary source of power in most satellites is from solar cells, a maximum number of the solar cells must be exposed to the sun at all times. The satellite antenna must also be pointed at the appropriate earth terminals. Our communications satellites use what is termed spin stabilization to meet these important requirements.

Spin stabilization operates on the principle that direction of the spin axis of a rotating body tends to remain fixed in space. An example of spin stabilization is the effect of the rotation of the earth in keeping its axis fixed in space. A satellite that has a spin axis parallel to the axis of the earth will maintain this position since both axes are fixed in space. Figure 4-8 illustrates the use of this principle. It depicts an equatorial orbit satellite used to keep a doughnut-shaped antenna pattern pointing toward the earth.

Figure 4-8 Spin-stabilized satellite antenna pattern

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4-11 UNCLASSIFIED Once the system is in motion, spin stabilization requires virtually no additional energy. A spin stabilized satellite is usually constructed like a flywheel. Its heavier equipment is mounted in the same plane and as close to the outside surface as possible.

After reaching its orbit, the radial jets are pulsed to start the satellite spinning. The satellite spin axis is orientated to the axis of the earth by means of small axial jets. Velocity jets are used to place the satellite in orbit position and provide velocity correction. Figure 4-9 is an example of spin stabilization.

Solar cells are installed around the outside surface of a spin-stabilized satellite. This gives you a large number of solar cells exposed to the sun at all times (except when the satellite is in eclipse). The use of omnidirectional antennas causes a small part of the total radiated energy to be directed toward the earth at all times.

Omnidirectional antennas radiate only a small amount of energy toward the earth. Many techniques have been tried to achieve an earth-oriented antenna system. One system developed uses spin stabilization for orientation of the satellite. It uses a stationary inner platform for mounting remote controlled antennas. The satellite is constructed in two parts with both parts having radial jets. The inner platform contains the communications antennas and the communications package. After the satellite is stabilized in space, inner radial jets spin the inner platform. The inner platform is stationary with respect to earth and is oriented to such a position that the communications antennas point continuously toward the earth. This arrangement allows the use of high-gain directional antennas that concentrate the majority of the radiated energy in the direction of the earth.

Figure 4-9 Spin-stabilized satellite controls

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4-12 UNCLASSIFIED The latest versions of communications satellites use a stationary platform with four high- gain antennas. Two steerable narrow beam antennas are used for communications between and within regions of high traffic density. Two horn antennas provide for earth communications between facilities outside the narrow beam coverage. The antenna arrangement for these types of communications satellites is shown in figure 4-7.

Q5. What was the major operational limitation of early communications satellites? Q6. Satellite orientation in space is important for what two reasons? 4.7 EARTH TERMINAL CHARACTERISTICS Communications satellite earth terminals are usually located in areas remote from the actual users of these communications. This is necessary to minimize rf interference to the satellite.

Locating the terminals in these remote locations requires interconnecting communications links. Links permit communications flow to and from the users of the satellite systems. Interconnect links are usually connected via telephone cables or microwave radio links with normal terminal equipment.

Earth satellite communications terminals generally have a single, large antenna; a highly sensitive receiver; a powerful transmitter; multiplex equipment; modulating- demodulating equipment; and telemetry equipment. Each of these elements will be discussed later in this chapter.

4.7.1 Antennas Earth terminal antennas are highly directional, high-gain antennas capable of transmitting and receiving signals simultaneously. Generally, large, high-gain, parabolic antennas are used.

Generally speaking, three sizes of parabolic-type antennas are currently in use at earth terminal sites. These are a parabolic antenna sixty feet in diameter, a parabolic antenna forty feet in diameter, and a cluster of four parabolic antennas, each ten feet in diameter. These four in combination are equal to a parabolic antenna eighteen feet in diameter. They are shown in figures 4-10, 4-11, and 4-12, respectively.

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4-13 UNCLASSIFIED

Figure 4-10 Typical satellite earth terminal with sixty-foot antenna Figure 4-11 Forty-foot antenna and pedestal

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4-14 UNCLASSIFIED

4.7.2 Receivers All satellite communications earth terminals are equipped with specially designed, highly sensitive receivers. These receivers are designed to overcome down-link power losses and to permit extraction of the desired communications information from the weak received signal. The terminals currently in use have specially designed preamplifiers mounted directly behind the antennas.

4.7.3 Transmitters All earth terminal transmitters generate high-power signals for transmission to the communications satellites. High-powered transmitters and highly directional, high-gain antennas are combined in this configuration. This is necessary to overcome up-link limitations and to ensure that the signals received by the satellite are strong enough to be detected by the satellite. Each transmitter has an exciter/modulator and a power amplifier. The modulator accepts the input signal from the terminal equipment and modulates an IF carrier. The exciter translates the IF signal to the up-link frequency and amplifies it to the level required by the power amplifier.

Figure 4-12 Parabolic antenna cluster

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4-15 UNCLASSIFIED Transmitters used in earth terminals have output power capabilities that vary from 10 watts to 20 kilowatts, depending on the type used and the operational requirements.

4.7.4 Telemetry Equipment Telemetry equipment is included in all communications satellite systems. This permits monitoring of the operating conditions within the satellite. Telemetry can be used also for remote control of satellite operations, such as energizing axial jets for changing the spin axis of the satellite.

Q7. What type of antennas are generally used at earth terminals? Q8. Why do earth terminals require highly sensitive receivers? Q9. What is the range of earth terminal transmitter output power? 4.8 SHIPBOARD RECEIVE-ONLY EQUIPMENT SYSTEMS The purpose of a shipboard receive-only system is to receive fleet multichannel teletypewriter broadcasts, which, as you recall from chapter 1, require no receipt. These are transmitted from a ground station and relayed to naval vessels by satellite.

Figure 4-13 is a typical shipboard receive-only system. In this system the transmitted carrier may be frequency modulated (fm) or phase-shift-key (psk) modulated for tty operation. The receiving antennas for this system are positioned about the ship. They are arranged in a manner (normally one in each quadrant of the ship) that at no time allows the line-of-sight to be blocked between the relay satellite and one or more of the antennas. Incoming signals pass from the antennas to an amplifier-converter. Each amplifier-converter routes an IF signal on one line of a twin axial cable that connects it to the combiner-demodulator. An operating power and local-oscillator signal are coupled from the combiner-demodulator to each amplifier-converter on the other line of the cable used for the IF signal. Because of signal path variations, shading, and reflections, the incoming signals are subject to random phase and amplitude variations.

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4-16 UNCLASSIFIED The combiner operation performed within the combiner-demodulator removes the phase variations from each input signal. It then measures the amplitudes of the signals for optimum combining and sums the signals. After being combined, the signal is demodulated and coupled from a receiver transfer switchboard to a telegraph demultiplex terminal.

Q10. What is the function of shipboard receive-only equipment? Q11. What types of modulation are shipboard receive-only equipment designed to receive?

Figure 4-13 Typical shipboard receive only system

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4-17 UNCLASSIFIED 4.9 SATELLITE ACQUISITION AND TRACKING An essential operation in communicating by satellite is the acquisition (locating) of the satellite by the earth terminal antenna and the subsequent tracking of the satellite. Initial acquisition depends upon an exact knowledge of the position of the satellite. In combination with the geographic location of the earth terminal, knowing the position of the satellite enables you to compute accurate antenna pointing information. The degree of difficulty in locating and tracking a satellite is determined largely by what type orbit the satellite is in.

The locating and tracking of a synchronous satellite is relatively simple. This is because the satellite appears to be stationary. Locating a near-synchronous satellite is also relatively simple because of the slow relative motion of the satellite However, the movement of a near-synchronous satellite is enough that accurate tracking is required to keep the narrow beam antenna pointed toward the satellite. Satellites in medium altitude circular orbits or in elliptical orbits are more difficult to acquire and to track because of the rapid changes in position.

4.9.1 Orbital Prediction To acquire and track a satellite in space, the earth terminal antennas must be provided with very accurate pointing information. Antenna pointing information is based upon the orbital prediction of the satellite. This information is derived from an EPHEMERIS table. This table provides the coordinates of a satellite or a celestial body at specific times during a given period. After you know the ephemeris data of a satellite, you can predict for any given location the apparent track of the satellite as viewed from that location.

The constants defining an orbit are initially obtained by the process of tracking. At the time of launch, the rocket is tracked by radar from lift-off to orbit and then until it passes out of sight. Tracking data obtained in this way is sufficient for making rough predictions of the orbit. These predictions are made rapidly with a computer and sent to tracking stations all over the world. These other tracking stations watch for the satellite during its first trip and record additional data. During the first week of orbiting, tracking stations all around the world are obtaining progressively more accurate data concerning the Satellite. This data is put into a computer where corrections of earlier estimates of the orbit are made.

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4-18 UNCLASSIFIED Once the initial predictions are complete and the satellite link becomes operational, very little change in these calculations is made. The orbits of a satellite will change slightly over a period of time; however, these changes are so gradual that predictions will be accurate enough to be used for weeks or even months without further corrections. When the orbits are known precisely, an ephemeris can be calculated for each satellite of the system.

4.9.2 Antenna Pointing Antenna pointing instructions for each satellite must be computed separately for each ground station location. A satellite that bears due south of station A at an elevation of 25 degrees may simultaneously bear due southeast of station B at an elevation of 30 degrees. Antenna pointing instructions are determined by taking into consideration the orbital prediction and the latitude and longitude of each ground station.

To establish radio contact with a satellite, the ground station needs to know the bearing and elevation of a satellite. This allows the antenna to be properly pointed.

4.9.3 Acquisition The acquisition of satellite signals by a ground station equipped with large antennas and operated at microwave frequencies places severe requirements on the system. Several factors must be considered. These factors are discussed below:

SPATIAL-TIME FACTOR.—Very accurate antenna pointing information is available to earth terminals from the satellite control facility located in Sunnyvale, California. Because of equipment limitations, a small search about the predicted location of the satellite must often be conducted to make initial contact. Either a manual or automatic scan is made around a small area close to the point where the satellite appearance is predicted.

FREQUENCY CONTROL.—The frequency of a radio signal received from a satellite is not generally the exact assigned down-link frequency. This variation depends upon the type of orbit of the satellite. The greatest frequency variations in signals from satellites occur in medium altitude circular or elliptical orbits. The smallest frequency variations occur in signals from satellites in near-synchronous or synchronous orbits.

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4-19 UNCLASSIFIED 4.9.4 Tracking When a particular satellite has been acquired, the earth terminal antenna will track that satellite for as long as it is used as a communications relay. Several methods of tracking are in actual use; however, we will explain PROGRAMMED TRACKING and AUTOMATIC TRACKING.

PROGRAMMED TRACKING.— In programmed tracking the known orbital parameters of the satellite are fed into computation equipment to generate antenna pointing angles. The antenna pointing angles are fed as commands to the antenna positioning servomechanisms. (You may want to review servos in NEETS, Module 15, Principles of Synchros, Servos, and Gyros.) These point the antenna in the required direction. The amount of data and computations involved in using programmed tracking is extensive. These are a result of the antenna mount flexing and atmospheric and ionospheric bending of radio waves. Because of these uncertainties, programmed tracking is not used extensively.

AUTOMATIC TRACKING.— In automatic tracking, the equipment generates antenna pointing information by comparing the direction of the antenna axis with the direction from which an actual satellite signal is received. Automatic tracking systems track the apparent position of a satellite. The direction of arrival of the radio signal and the real position of the satellite is not required. The automatic tracking system uses a servomechanism to move the antenna. Once the satellite has been located, the servomechanism generates its own pointing data. This eliminates the requirement for continuous data input and computation.

SATELLITE OUTAGE TIME.—The satellite outage time specifications allow for stewing (moving) the earth terminal antennas, acquiring the satellite signal, and checking for circuit continuity at HAND OVER. (Hand over is the period of time for one earth terminal to yield control to another as a satellite moves out of its area of coverage.) This hand over period represents an outage time. If the control terminal is unable to hand over to another terminal within a specified time, other arrangements are made. For example, control may be retained or transferred to another terminal within the coverage area. There are several reasons why a terminal may be unable to assume control on time; these reasons may combine to increase the outage time. The difference of drift velocities of the satellites leads to bunching within a coverage area. This causes gaps in coverage and increases outage times. When two or more satellites simultaneously occupy the same space of the terminal antennas, they will interfere with each other.

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4-20 UNCLASSIFIED This prevents reliable communications. Other factors leading to increased outage times are SATELLITE-SUN CONJUNCTION (increased noise while the satellite passes near the sun), SATELLITE ECLIPSE (absence of power from solar cells), and satellite failures. The distribution of outage times is a complicated function of time and earth- station locations. With careful coverage coordination, maximum communications effectiveness is obtained.

Q12. Why is satellite acquisition and tracking important? 4.10 ROLE OF SATELLITE COMMUNICATIONS In the context of a worldwide military communications network, satellite communications systems are very important. Satellite communications links add capacity to existing communications capabilities and provide additional alternate routings for communications traffic. Satellite links, as one of several kinds of long-distance links, interconnect switching centers located strategically around the world. They are part of the defense communication systems (DCS) network. One important aspect of the satellite communications network is that it continues in operation under conditions that sometimes render other methods of communications inoperable. Because of this, satellites make a significant contribution to improved reliability of Navy communications.

4.10.1 Advantages of Satellite Communications Satellite communications have unique advantages over conventional long distance transmissions. Satellite links are unaffected by the propagation variations that interfere with hf radio. They are also free from the high attenuation of wire or cable facilities and are capable of spanning long distances. The numerous repeater stations required for line- of-sight or troposcatter links are no longer needed. They furnish the reliability and flexibility of service that is needed to support a military operation.

4.10.1.1 Capacity The present military communications satellite system is capable of communications between backpack, airborne, and shipboard terminals. The system is capable of handling thousands of communications channels.

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4-21 UNCLASSIFIED 4.10.1.2 Reliability Communications satellite frequencies are not dependent upon reflection or refraction and are affected only slightly by atmospheric phenomena. The reliability of satellite communications systems is limited only by the equipment reliability and the skill of operating and maintenance personnel.

4.10.1.3 Vulnerability Destruction of an orbiting vehicle by an enemy is possible. However, destruction of a single communications satellite would be quite difficult and expensive. The cost would be excessive compared to the tactical advantage gained. It would be particularly difficult to destroy an entire multiple-satellite system such as the twenty-six random-orbit satellite system currently in use. The earth terminals offer a more attractive target for physical destruction. These can be protected by the same measures that are taken to protect other vital installations.

A high degree of freedom from jamming damage is provided by the highly directional antennas at the earth terminals. The wide bandwidth system that can accommodate sophisticated anti-jam modulation techniques also lessens vulnerability.

4.10.1.4 Flexibility Most operational military satellite earth terminals are housed in transportable vans. These can be loaded into cargo planes and flown to remote areas. With trained crews these terminals can be put into operation in a matter of hours. Worldwide communications can be established quickly to remote areas nearly anywhere in the free world.

4.10.2 Satellite Limitations Limitations of a satellite communications system are determined by the technical characteristics of the satellite and its orbital parameters. Active communications satellite systems are limited by two things. Satellite transmitter power on the down links and receiver sensitivity on the up links. Some early communications satellites have been limited by low-gain antennas.

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4-22 UNCLASSIFIED 4.10.2.1 Power The amount of power available in an active satellite is limited by the weight restrictions imposed on the satellite. Early communications satellites were limited to a few hundred pounds because of launch vehicle payload restraints. The only feasible power source is the inefficient solar cell. (Total power generation in the earlier satellites was less than 50 watts.) As you can see, the rf power output is severely limited; therefore, a relatively weak signal is transmitted by the satellite on the down link. The weak transmitted signal is often reduced by propagation losses. This results in a very weak signal being available at the earth terminals. The level of signals received from a satellite is comparable to the combination of external atmospheric noise and internal noise of standard receivers. Special techniques must be used to extract the desired information from the received signal. Large, high-gain antennas and special types of preamplifiers solve this problem but add complexity and size to the earth terminal. (The smallest terminal in the defense communication systems network has effectively an 18-foot antenna and weighs 19,500 pounds.) Development of more efficient power sources and relaxation of weight restrictions have permitted improved satellite performance and increased capacity.

4.10.2.2 Receiver Sensitivity Powerful transmitters with highly directional antennas are used at earth stations. Even with these large transmitters, a lot of signal loss occurs at the satellite. The satellite antenna receives only a small amount of the transmitted signal power. A relatively weak signal is received at the satellite receiver. This presents little problem as the strength of the signal received on the up link is not as critical as that received on the down link. The down-link signal is critical because the signal transmitted from the satellite is very low in power. Development of high-gain antennas and highly sensitive receivers have helped to solve the down-link problem.

4.10.2.3 Availability The availability of a satellite to act as a relay station between two earth terminals depends on the locations of the earth terminals and the orbit of the satellite. All satellites, except those in a synchronous orbit, will be in view of any given pair of earth stations only part of the time. The length of time that a nonsynchronous satellite in a circular orbit will be in the ZONE OF MUTUAL VISIBILITY (the satellite can be seen from both terminals) depends upon the height at which the satellite is circling. Elliptical orbits cause the satellite zone of mutual visibility between any two earth terminals to vary from orbit to orbit. These times of mutual visibility are predictable. Figure 4-14 illustrates the zone of mutual visibility.

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4-23 UNCLASSIFIED

Q13. What are the two limitations to an active satellite communications system? 4.10.3 Future Satellite Communications Satellite communications are becoming well established in the Navy. In October 1983 the Department of the Navy established the Naval Space Command, which assumed operational responsibility for Navy space systems plus coordination responsibility with other operational activities. Most ships have satellite communications capability. New systems have been installed on ships and are fully compatible with other electronic systems and equipment. Communications via satellite has increased existing Navy communications capabilities for the command and control of naval forces. Satellite communications has not replaced all existing means of radio communications. However, it is a major step in modernizing Navy communications. It has relieved the Navy of its total dependence on hf radio transmission and reduced the need for many hf ground stations overseas.

Figure 4-14 Zone of mutual visibility

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4-24 UNCLASSIFIED A recent step in the advancement of satellite communications was the start of the DSCS Phase III. The first Phase III satellite was launched into orbit by the space shuttle in the summer of 1984. Seven satellites will be placed in space during this phase. Figure 4-15 shows a Phase III satellite being tested in a simulated space environment, Figure 4-16 shows the Phase III satellite as it appears in space. Phase III will develop the use of 40- watt, solid-state amplifiers to replace the currently used traveling-wave tube (twt). It will also be used to develop new type filters. These filters will provide increased channel bandwidth, which will provide additional communications capacity.

Figure 4-15 DSCS Phase III satellite being tested

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4-25 UNCLASSIFIED

The survivability of reliable communications for the command and control of our strategic nuclear forces is paramount. Space systems perform many missions more effectively than earthbound systems.

Spaceborne communications increase the effectiveness of military operations. The Department of Defense is engaged in the development of new communications techniques and systems, including some that are space based. As the use of space continues its march forward, vital new opportunities for national defense will continue to materialize. This will improve the survivability of our strategic communications against nuclear and electronic attack.

More information on satellite communications can be found in Navy publication NTP 2, Navy Satellite Operations. This publication was written to concisely explain the role of the Navy in the Defense Communications Satellite Program. It also issues procedures for effective, coordinated use of available satellite resources.

4.11 SUMMARY Now that you have completed this chapter, a short review of what you have learned will be helpful. The following review will refresh your memory of satellite communications, equipment, and theory.

A PASSIVE SATELLITE is one that reflects radio signals back to earth.

An ACTIVE SATELLITE is one that amplifies the received signal and retransmits it back to earth.

REPEATER is another name for an active satellite.

The UP LINK is the frequency used to transmit a signal from earth to a satellite.

Figure 4-16 DSCS Phase III satellite as it appears in space

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4-26 UNCLASSIFIED The DOWN LINK is the frequency used to transmit an amplified signal from the satellite back to earth.

A SYNCHRONOUS ORBIT is one in which the satellite moves or rotates at the same speed as the earth.

An ASYNCHRONOUS ORBIT is one where the satellite does not rotate or move at the same speed as the earth.

A NEAR SYNCHRONOUS ORBIT is one in which the satellite rotates close to but not exactly at the same speed as the earth.

PERIGEE is the point in the orbit of a satellite closest to the earth.

APOGEE is the point in the orbit of a satellite the greatest distance from the earth.

The ANGLE OF INCLINATION is the angular difference between the equatorial plane of the earth and the plane of orbit of the satellite.

INCLINED ORBITS are orbits where there is some amount of inclination. These include equatorial and polar orbits.

An EQUATORIAL ORBIT is an orbit that occurs when the plane of a satellite coincides with the plane of the earth at the equator.

A POLAR ORBIT is an orbit that has an angle of inclination of or near 90 degrees.

A MEDIUM ALTITUDE ORBIT is an orbit from 2,000 to 12,000 miles above the earth. The rotation rate of the earth and satellite are quite different, and the satellite moves quickly across the sky.

An ECLIPSE is when the satellite is not in view or in direct line of sight with the sun. This happens when the earth is between them.

An EPHEMERIS is a table showing the precalculated position of a satellite at any given time.

PROGRAMMED TRACKING uses known satellite orbital parameters to generate antenna pointing angles.

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4-27 UNCLASSIFIED AUTOMATIC TRACKING is done by the equipment comparing the direction of the antenna axis and the direction of the received signal.

HAND OVER is the period of time for one earth terminal to yield control to another as a satellite moves out of its area of coverage.

SATELLITE-SUN CONJUNCTION is when the satellite and sun are close together and the noise from the sun prevents or hampers communications.

A SATELLITE ECLIPSE is an eclipse where the rays of the sun don't reach the satellite. This prevents recharging of the solar cells of the satellite and decreases the power to the transmitter.

The ZONE OF MUTUAL VISIBILITY is where the satellite can be seen by both the up- and down-link earth terminals.

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4-28 UNCLASSIFIED ANSWERS TO QUESTIONS Q1. THROUGH Q13. A1. Passive and active.

A2. Earth terminals.

A3. Approximately one-half.

A4. The extreme polar regions.

A5. The lack of suitable power sources.

A6. To allow maximum solar cell exposure to the sun and satellite antenna exposure to earth terminals.

A7. Large, high-gain parabolic antennas.

A8. To overcome satellite transmitter low power and permit extraction of the desired information from the received signal.

A9. Up to 20 kilowatts.

A10. To receive fleet multichannel tty broadcasts.

A11. Fm or psk.

A12. To ensure earth terminal antennas are always pointed towards the satellite.

A13. Satellite down-link transmitter power and up-link receiver sensitivity.

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