METHOD FOR MISSILE CONTROL (MODIFICATIONS) AND MISSILE CONTROL SYSTEM FOR ITS REALIZATION (MODIFICATIONS) Russian patent published in 2007 - IPC F42B15/01 F41G7/20 

FIELD: armament, in particular, rocketry, applicable in development of missile complexes, for example, with carriers on the ground in which beam guidance systems, homing systems are used.

SUBSTANCE: two methods of missile control are offered, in which the value of the angular velocity of the missile axis in one plane (for example, in pitching) is measured, or in two planes (in pitching and heading) respectively converted to on electric signal, from which at the frequency of natural oscillations of the missile a signal proportional to the amplitude of the respective natural oscillations is discriminated. Their value forms the value of the compensating command (or commands) summed up with command (or commands) from which the missile control command (commands) is (are) formed. The missile (first modification) is provided in one of the channels with an angular-rate sensor, oscillations discrimination device and a compensating command shaper. The missile (the second modification) is provided with the second adder, and each channel of the first and second circuits includes an angular-rate sensor, use is also made of a discrimating device of oscillations and a compensating command shaper.

EFFECT: enhanced reliability.

4 cl, 2 dwg