Collision Avoidance System for Unmanned Aerial Vehicle (UAV)
controller principally works by driving the cross-track and course angle errors of the UAV flight, relative to the desired path, to zero, through performing Bank to Turn (BTT) maneuvers. The system generates corrective commands, based on the error information, and transforms it into a heading change via roll maneuver. The roll maneuver controller is designed using LQR technique such that it can provide an appropriate roll
dynamics of the UAV. Simulation results will be presented and analyzed to investigate the performance of the proposed system.
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