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INFLUENCE OF SYSTEM INPUTS ON THE DESIGN
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acceleration command aerodynamics altitude analog computer analog simulation angles of attack apparent line-of-sight assumed attack situation autopilot command average miss distance block diagram body angular velocity considered constant control system gain effects of radome electromagnetic radiation employed equation fast autopilot filtering ft/sec gate closes gate control gate level gating signal glint noise high altitudes hold circuit initial heading error integrator intercept k-Compensation circuit line-of-sight angle line-of-sight information line-of-sight rate look angle loop gain magnitude missile acceleration missile control system missile maneuver modified system open-loop gain perfectly compensated system performance pitch channel pitch rate problem quantity radar dynamics radar output radian/radian radian/sec radians radome diffraction feedback radome diffraction perturbation radome error slope random target maneuver rate gyro result sample-and-hold circuit seen shown in figure simulation study sketch sluggish system step command step response system inputs time-varying gain transfer function transient trial-and-error Typical trajectories volts normalized WADC