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Inverse kinematics in ultralight UAV control problem with additional on-board microcomputer.

Konstantin Amelin, Vasiliy Kaliteevskiy, Zeev Volkovich
The architecture of the autopilot control unit for the UAV is given. The possibility of using additional on-board microcomputer for collaboration with the autopilot to increase functionality of UAV is considered. The microcomputer TRIK is used. The dinamic and kinematic of flight process are described. Several coordinate systems for describe the dynamic behaviors of UAV are given. The method of partly implement the autopilot systems control modules to microcomputer is proposed. Simulation results of motions model in Simulink are described. Testing the proposed module on the real UAV is planned.
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