METHOD AND SYSTEM OF GUIDANCE OF SPIN-STABILIZED MISSILE BY FREQUENCY LASER RADIATION REFLECTED FROM TARGET

摘要

FIELD: armament, in particular, artillery guided missiles with laser guidance.;SUBSTANCE: target lighting is switched on at the final section of the trajectory, then analog signals are formed with the aid of the optoelectronic correction head. These signals are numbered and introduced in a microprocessor for computation of the missile angular velocity spin, as well as of the value and phase of the miss. According to the number of the impulse vernier engine selected by the program, the signal of its starting is formed at the time instant computer with due account made for the tubular dependence of the corrective pulse length on the engine powder charge. The guidance system has functional units and circuits required for realization of the method.;EFFECT: enhanced accuracy and simplified guidance system.;2 cl, 3 dwg