Hidetaka Takano

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A guidance and control system for a trajectory-tracking unmanned aerial vehicle (UAV) is introduced. A proportional navigation guidance law is applied to a trajectory-tracking flight instead of using a traditional tracking-error correction based method. The system employs a dynamic inversion technique for the guidance force generation, which allows the UAV(More)
Maneuverability of aircraft, particularly high-performance aircraft, has been improved remarkably, which include the poststall maneuverability and the thrust vectoring. However, the performance of the aircraft is shown well only when the aircraft carry out the best maneuvers. In this paper, we try to optimize the vertical loop of the aircraft with poststall(More)
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