MATHEMATICAL MODELING OF THE OPERATION OF AN AIRCRAFT GYROSCOPE
Keywords:
missile, drone, flight, system, guidance, homing, angular motion.Abstract
A dynamically tuned gyroscope used in a compact gyroscopic angular velocity vector meter of an aircraft is considered. Guided missile inclination methods are analyzed. Mathematical models of the gyroscope rotor motion on a fixed base and the angular motion of the aircraft missile gyroscope itself are presented.
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