FIELD: aviation.
SUBSTANCE: simulation model of a system for control of an air target based on an unmanned aerial vehicle of a target complex contains autopilot contours for control of lateral and longitudinal movements of the air target based on UAV. The contour for control of the lateral movement of the autopilot contains a sub-contour for control of a course angle of the air target with subsequent closure with a sub-contour for control of roll of the air target and has an amplification coefficient of a differential adjuster of damping a roll speed for an inner contour. The contour for control of the longitudinal movement contains feedback sub-contours: a sub-contour for maintenance of a flight height of the air target based on UAV, using control signals, by pitch with subsequent closure with a sub-contour of the autopilot for stabilization by a pitch angle, used as an inner sub-contour, a sub-contour for maintenance of a speed of the air target based on UAV, using adjustment of pitch, a sub-contour for stabilization of the speed of the air target based on UAV, using a throttle valve, which also have units implementing corresponding amplification coefficients.
EFFECT: provision of checking of technical solutions of a system for control of an air target, using a simulation model.
1 cl, 14 dwg
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Authors
Dates
2022-10-21—Published
2020-05-25—Filed