CONTROL BY THE MANEUVER OF AN UNMANNED AERIAL VEHICLE WHEN LANDING ON A MOBILE PLATFORM USING THE METHOD OF "FLEXIBLE" KINEMATIC TRAJECTORIES
Annotation
The task of synthesis of an algorithm for control of terminal maneuver of aircraft–type UAV landing on a mobile platform is formulated and accomplished by the method of reverse dynamics problems using the principles of flexible kinematic trajectories and pointing to the landing point. Results of the synthesized control algorithm for the landing maneuver of the UAV Aerosonde testing in the MATLAB environment for various wind disturbances are presented.
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