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Aircraft and Missile Guidance and Trajectory Control
Introduction to Radar and ElectroOptical Homing Systems
Target Detection in Radar Guidance Systems
6 other sections not shown
acceleration accelerometers aircraft algorithm amplifier amplitude analog angle tracker angle-sensing angular velocity antenna automatic control system axis bandwidth block diagram channel characterizes circuit closing velocity clutter coefficients components compound sensor condition constant control surface control vector correction signal damper detection system determined device discriminator doppler frequency dynamic error error signal estimate feedback FIGURE frequency modulation g-force gating pulses guidance system homing loop homing systems impulse response inertial input integrator interceptor Kalman filtering kinematic line of sight linear matrix mean square error measurement system missile guidance missile seeker modulation motion normal obtain operation optimum control oscillations performed phase phase detectors pilot pitch problem pulsed doppler radar range and velocity range cell range measurement root mean square semiactive shown in Fig spectral density target angle target signal threshold tracking system trajectory control transfer function variance vector vertical plane voltage white noise