• جزئیات بیشتر مقاله
    • تاریخ ارائه: 1392/07/24
    • تاریخ انتشار در تی پی بین: 1392/07/24
    • تعداد بازدید: 1180
    • تعداد پرسش و پاسخ ها: 0
    • شماره تماس دبیرخانه رویداد: -
      this paper presents an integrated guidance and control design scheme for an unmanned airvehicle (uav), and its flight test results. the paper focuses on the longitudinal control and guidance aspects, with particular emphasis on the terrain-following problem. an introduction to the mission, and the terrain-following problem is given first. waypoints for climb and descent are defined. computation of the reference trajectory in the vertical plane is discussed, including a terrain-following (tf) algorithm for real-time calculation of climb/descent points and altitudes. the algorithm is particularly suited for online computation and is therefore useful for autonomous flight. the algorithm computes the height at which the vehicle should fly so that a specified clearance from the underlying terrain is always maintained, while ensuring that the vehicle’s rate of climb and rate of descent constraints are not violated. the output of the terrain-following algorithm is used to construct a smooth reference trajectory for the vehicle to track. the design of a robust controller for altitude tracking and stability augmentation of the vehicle is then presented. the controller uses elevators for pitch control in the inner loop, while the reference pitch commands are generated by the outer altitude control loop. the controller tracks the reference trajectory computed by the terrain-following algorithm. the design of an electromechanical actuator for actuating the control surfaces of the vehicle during flight is also discussed. the entire guidance and control scheme is implemented on an actual experimental vehicle and flight test results are presented and discussed.

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