

Electronic Warfare and Radar Systems Engineering Handbook  Modulation (Title) 

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MODULATION
Modulation is the process whereby some characteristic of one wave is varied in accordance with some
characteristic of another wave. The basic types of modulation are angular modulation (including the special cases
of phase and frequency modulation) and amplitude modulation. In missile radars, it is common practice to amplitude
modulate the transmitted RF carrier wave of tracking and guidance transmitters by using a pulsed wave for
modulating, and to frequency modulate the transmitted RF carrier wave of illuminator transmitters by using a sine
wave.
Frequency Modulation (FM)  As shown in Figure 1, an unmodulated RF signal in the time domain has only a single
spectral line at the carrier frequency (fc) in the frequency domain. If the signal is frequency modulated, as
shown in Figure 2, the spectral line will correspondingly shift in the frequency domain.
Amplitude
Modulation (AM)  If the signal in Figure 1 is amplitude modulated by a sinewave as shown in Figure 3, sidebands
are produced in the frequency domain at Fc ± FAM. AM other than by a pure sine wave will cause additional
sidebands normally at Fc ± n_{FAM}, where n equals 1, 2, 3, 4, etc.
Pulse modulation is a special case of AM wherein the carrier frequency is gated at a pulsed rate. When the
reciprocal of the duty cycle of the AM is a whole number, harmonics corresponding to multiples of that whole
number will be missing, e.g. in a 33.33% duty cycle, AM wave will miss the 3rd, 6th, 9th, etc. harmonics, while a
square wave or 50% duty cycle triangular wave will miss the 2nd, 4th, 6th, etc. harmonic, as shown in Figure 4. It
has sidebands in the frequency domain at Fc ± n_{FAM}, where n = 1, 3, 5, etc. The amplitude of the power
level follows a sine x / x type distribution.
Figure
5 shows the pulse width (PW) in the time domain which defines the lobe width in the frequency domain (Figure 6).
The width of the main lobe is 2/PW, whereas the width of a side lobe is 1/PW. Figure 5 also shows the pulse
repetition interval (PRI) or its reciprocal, pulse repetition frequency (PRF), in the time domain. In the
frequency domain, the spectral lines inside the lobes are separated by the PRF or 1/PRI, as shown in Figures 7 and
8. Note that Figures 7 and 8 show actual magnitude of the side lobes, whereas in Figure 4 and 6, the absolute
value is shown.
The magnitude of each spectral component for a rectangular pulse can be determined from the
following formula:
[1]
Figure 7 shows the spectral lines for a square wave (50% duty cycle), while Figure 8 shows the spectral lines
for a 33.33% duty cycle rectangular wave signal.
Figure
9 shows that for square wave AM, a significant portion of the component modulation is contained in the first few
harmonics which comprise the wave. There are twice as many sidebands or spectral lines as there are harmonics (one
on the plus and one on the minus side of the carrier). Each sideband represents a sine wave at a frequency equal
to the difference between the spectral line and fc .
A figure similar to Figure 9 can be created for any
rectangular wave. The relative amplitude of the time domain sine wave components are computed using equation [1].
Each is constructed such that at the midpoint of the pulse the sine wave passes through a maximum (or minimum if
the coefficient is negative) at the same time. It should be noted that the "first" harmonic created using this
formula is NOT the carrier frequency, fc , of the modulated signal, but at Fc ± FAM.
While equation [1] is for rectangular waves only, similar equations can be constructed using Fourier coefficients
for other waveforms, such as triangular, sawtooth, half sine, trapezoidal, and other repetitive geometric shapes.
PRI Effects  If the PW remains constant but PRI increases, the number of sidelobes remains the same, but the
number of spectral lines gets denser (move closer together) and vice versa (compare Figure 7 and 8). The spacing
between the spectral lines remains constant with constant PRI.
Pulse Width (PW) Effects  If the PRI
remains constant, but the PW increases, then the lobe width decreases and vice versa. If the PW approaches PRI,
the spectrum will approach "one lobe", i.e., a single spectral line. The spacing of the lobes remains constant
with constant PW.
RF Measurements  If the receiver bandwidth is smaller than the PRF, the receiver will
respond to one spectral line at a time. If the receiver bandwidth is wider than the PRF but narrower than the
reciprocal of the PW, the receiver will respond to one spectral envelope at a time.
Jet Engine Modulation
(JEM)
Section
26 addresses the Doppler shift in a transmitted radar signal caused by a moving target. The amount of Doppler
shift is a function of radar carrier frequency and the speed of the radar and target. Moving or rotating surfaces
on the target will have the same Doppler shift as the target, but will also impose AM on the Doppler shifted
return (see Figure 10).
Reflections off rotating jet engine compressor blades, aircraft propellers, ram air turbine (RAT) propellers
used to power aircraft pods, helicopter rotor blades, and protruding surfaces of automobile hubcaps will all
provide a chopped reflection of the impinging signal. The reflections are characterized by both positive and
negative Doppler sidebands corresponding to the blades moving toward and away from the radar respectively.
Therefore, forward/aft JEM doesn't vary with radar carrier frequency, but the harmonics contained in the sidebands
are a function of the PRF of the blade chopping action and its amplitude is target aspect dependent, i.e. blade
angle, intake/exhaust internal reflection, and jet engine cowling all effect lateral return from the side. If the
aspect angle is too far from headon or tailon and the engine cowling provides shielding for the jet engine,
there may not be any JEM to detect. On the other hand, JEM increases when you are orthogonal (at a right angle) to
the axis of blade rotation. Consequently for a fully exposed blade as in a propeller driven aircraft or
helicopter, JEM increases with angle off the boresight axis of the prop/rotor.
Table of Contents
for Electronics Warfare and Radar Engineering Handbook
Introduction 
Abbreviations  Decibel  Duty
Cycle  Doppler Shift  Radar Horizon / Line
of Sight  Propagation Time / Resolution  Modulation
 Transforms / Wavelets  Antenna Introduction
/ Basics  Polarization  Radiation Patterns 
Frequency / Phase Effects of Antennas 
Antenna Near Field  Radiation Hazards 
Power Density  OneWay Radar Equation / RF Propagation
 TwoWay Radar Equation (Monostatic) 
Alternate TwoWay Radar Equation 
TwoWay Radar Equation (Bistatic) 
Jamming to Signal (J/S) Ratio  Constant Power [Saturated] Jamming
 Support Jamming  Radar Cross Section (RCS) 
Emission Control (EMCON)  RF Atmospheric
Absorption / Ducting  Receiver Sensitivity / Noise 
Receiver Types and Characteristics 
General Radar Display Types 
IFF  Identification  Friend or Foe  Receiver
Tests  Signal Sorting Methods and Direction Finding 
Voltage Standing Wave Ratio (VSWR) / Reflection Coefficient / Return
Loss / Mismatch Loss  Microwave Coaxial Connectors 
Power Dividers/Combiner and Directional Couplers 
Attenuators / Filters / DC Blocks 
Terminations / Dummy Loads  Circulators
and Diplexers  Mixers and Frequency Discriminators 
Detectors  Microwave Measurements 
Microwave Waveguides and Coaxial Cable 
ElectroOptics  Laser Safety 
Mach Number and Airspeed vs. Altitude Mach Number 
EMP/ Aircraft Dimensions  Data Busses  RS232 Interface
 RS422 Balanced Voltage Interface  RS485 Interface 
IEEE488 Interface Bus (HPIB/GPIB)  MILSTD1553 &
1773 Data Bus  This HTML version may be printed but not reproduced on websites.



