FIELD: flying vehicle control systems; aeronautical engineering and rocketry.
SUBSTANCE: proposed system includes pitch, heading and roll channels whose inputs are connected with inputs of system by control signals, signals of two-degree-of-freedom gyroscopes and angular velocity sensors. Proposed system also includes kinematic wiring unit which includes inverters, adders and actuators. Pitch, heading and roll channels are provided with functional converters, limiting parameter setter and comparator.
EFFECT: improved dynamic properties of system; extended functional capabilities.
6 dwg
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