Tighter beam means more gain — and less coverage per scan position
Block 1 · Lesson 6 · Part Two
Steering Without Moving
Replace one dish with many small radiators, and the beam is pointed by arithmetic instead of by a motor.
Block 1 · Lesson 6 · Beamforming
Beamforming Basics
Replace the dish with $N$ small radiators (an array). Each element transmits the same signal with a programmed phase $\phi_n$.
Progressive phase
\[ \Delta \phi = \frac{2\pi}{\lambda} \, d \, \sin\theta_s \]
Constructive interference at the steering angle $\theta_s$ $\Rightarrow$ main lobe points there
Beam steered electronically — no moving parts
More elements $\Rightarrow$ narrower beam and lower side lobes (with tapering)
Space them too far apart and the pattern aliases — grating lobes, full-strength copies pointing where you did not ask: $d \le \lambda / (1 + |\sin\theta_0|)$
Block 1 · Lesson 6 · Scan Loss
Pointed at Boresight, the Array Is at Its Best
Load a flat phase across the elements and the beam sits at $\theta_0 = 0$ — the array shows the target its full aperture.
Every element is broadside to the target, so the projected aperture is the whole array.
Block 1 · Lesson 6 · Scan Loss
Steer It to 60°, and Physics Sends a Bill
Nothing moved. But the target now sees the array edge-on, so the effective aperture shrinks as $\cos\theta_0$ — and a smaller aperture makes a wider beam.
was here$\theta_0 = 0^\circ$
$\theta_0 = 60^\circ$beamwidth $2\theta_B$ · about $-3$ dB
−90°
−60°
−30°
0°
30°
60°
90°
HPBW broadens as $1/\cos\theta_0$ — at $60^\circ$ that is twice as wide
Effective aperture drops by $\cos 60^\circ = 0.5$, costing about 3 dB of gain
An ESA is worst exactly where it is scanning hardest.
Block 1 · Lesson 6 · ESA / AESA
Electronically Scanned Arrays (ESA / AESA)
ESA $=$ beam steered by phase shifters. AESA $=$ active ESA, each element has its own Tx/Rx module.
What it does
What it buys the threat
Microsecond beam pointing
Track many targets; interleave search and track in one dwell
Graceful degradation
A few failed modules cost a few percent gain, not the radar
Multi-beam
Different waveforms in different directions at the same time
HPBW still broadens as $1/\cos\theta_s$ off boresight — physics does not care how modern the array is
Modern fire control radars and most new IADS surveillance are AESA
Block 1 · Lesson 6 · Why It Matters
Why Patterns Matter for EW
Side-lobe leak — a jammer not on boresight still enters through side lobes
EP response: side-lobe cancellation, side-lobe blanker, low-SLL antennas
Main-beam pointing — knowing where the threat is looking tells you what it is doing
ESA agility — compresses the threat's kill chain; harder to deceive with classical techniques
Polarization purity — cross-pol leakage shows up in patterns and matters for LO
Side lobes are the back door for EW.
Today's Interactive Demo: Phased Array Simulator
Companion script:L6_ArrayFactorAndSteering.m
In L7 we put these patterns inside an IADS and watch each radar do its job
Live demo
Phased Array Simulator
usafa-ece.github.io/ece-495-ew
Block 1 · Lesson 6 · Type-along
Your Turn
Laptops open, MATLAB up. Ten lines that add up phasors, one parameter changed, and a claim from the last slide put to the test.
Block 1 · Lesson 6 · Quick Exercise
Quick Exercise / Type-along: Walk the Grating Lobe
Eight elements, wide spacing. Type it, run it — then change th0 to 30 and run it again.
N = 8; dlam = 0.9; th0 = 0; % elements, d/lambda, steer (deg)
th = -90:0.25:90; % look angles (deg)
n = (0:N-1).'; % element index, as a column
beta = -2*pi*dlam*sind(th0); % programmed phase per element
AF = sum(exp(1j*n*(2*pi*dlam*sind(th) + beta)), 1)/N;
plot(th, 20*log10(max(abs(AF),1e-3)), 'LineWidth',1.5);
hold on; grid on; ylim([-40 0]);
xlabel('theta (deg)'); ylabel('|AF| (dB)');
fprintf('theta0=%2d | beta=%7.1f deg/elem | limit %.2f | used %.2f\n', ...
th0, rad2deg(beta), 1/(1+abs(sind(th0))), dlam);
Full-strength lobes at $\theta_0 = 0$? At $\theta_0 = 30^\circ$?
The spacing never changed. What did?
Block 1 · Lesson 6 · Wrap-Up
Wrap-Up
Key ideas
Patterns have main, side, and back lobes; side lobes are the EW back door
HPBW $\propto \lambda / D$; gain $\propto$ aperture $/ \lambda^2$
ESA / AESA $=$ microsecond beam steering, multi-beam, graceful degradation
Next lesson
L7: Threat radar taxonomy in an IADS — EW, ACQ, HF, GCI, TTR, AI, TIR
Work the L7 pre-flight before class — you could be the one up front