FIELD: military equipment.
SUBSTANCE: invention relates to the field of automatic control systems, namely to systems for automatic guidance and stabilization of a package of guides with rockets placed on a combat vehicle of a multiple rocket reaction system. System includes an adjustable pump with a cage position sensor, a hydraulic tank, a hydraulic motor, a guide package, summing amplifiers, an error generator, a pressure sensor, throttling solenoid valves, hydraulic cylinders, absolute position and absolute speed sensors, frequency-dependent functional blocks, multipliers, bandpass filters, module isolation units, scaling links, adders, integrator, bipolar comparators.
EFFECT: accuracy characteristics of the guidance and stabilization system of the guide package are increased due the change in the gain factors along the positioning contours and the velocity in horizontal and vertical stabilization channels.
1 cl, 2 dwg
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Authors
Dates
2018-10-16—Published
2017-08-11—Filed