The paper analyzes the transformation of the movement of the tracking optoelectric system in a selected phase of flight in the longitudinal plane. Mathematical models of this integrated system are described by transfer functions, which are transferred to the state space with evaluation in the MATLAB/Simulink simulation environment. The control of an automatic tracking system on an aircraft is determined in the direction of the tracking line with its mutual symmetry between two objects. A gyroscope is placed on the tracking system, the function of which is to measure the angular velocities of the tracking line. The output of the tracking optoelectronic system is the angular velocity of the tracking system line control, which is the main input to the prediction computer for calculating the take-off angle and to control the aircraft system to provide a command to increase dynamics in the tilt position control system.
Control of the Airplane Sighting System
2021-11-25
1933524 byte
Conference paper
Electronic Resource
English
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