FIELD: automatic control system.
SUBSTANCE: invention relates to the field of automatic control systems and can be used in guidance and stabilization systems of weapons and optoelectronic devices of infantry combat vehicles, antiaircraft-missile and antiaircraft-rocket-gun complexes. Essence of the disclosed solution lies in the fact that a guidance and stabilization system comprising a first integrator, series-connected adder, adder amplifier, power amplifier and actuating motor, a first rate gyroscope, a second rate gyroscope, a first multiplier unit, first input of which is connected to second rate gyroscope output, second input is connected to first integrator output, second integrator, input of which is connected to first multiplier output, second multiplier, first input of which is connected to second rate gyroscope output, second input is connected to second integrator output, and output is connected to adder second input, wherein adder first input is connected to first integrator output, the output of the first rate gyroscope and the output of the rate generator are connected to the second and third inputs of the summing amplifier, the rate generator input is mechanically connected to the output of the actuator.
EFFECT: technical result when implementing disclosed solution consists in improvement of stabilization accuracy.
1 cl, 1 dwg
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Authors
Dates
2020-11-09—Published
2020-03-03—Filed