SELF-OSCILLATING AUTOMATIC PILOT OF GUIDED MISSILE Russian patent published in 1998 - IPC

FIELD: defensive technology. SUBSTANCE: technical result of invention is achieved by series connection in self-oscillating automatic pilot of subtracter which first input is mission input of automatic pilot, of correction filter of integrodifferentiating type with prevalence of integration on self-oscillation frequencies and limiting elements built on operational amplifier, of relay element, of power amplifier and guiding machine with controlling magnet which output is output of automatic pilot and is connected through feedback pickup to second input of subtracter. Mission input of automatic pilot is connected to controlling input of relay element. EFFECT: enhanced speed of response of automatic pilot ( diminished time of turn of rudders from zero position to maximum angle ) and provision for maximum angle of turn of rudders by rests while automatic pilot responds to pulse control signals. 3 dwg