本文選題：準平衡滑翔 + 在線軌跡規(guī)劃�。� 參考：《航天控制》2016年05期

【摘要】：針對飛行器在線軌跡規(guī)劃問題提出一種基于準平衡滑翔條件的軌跡在線規(guī)劃方法及利用PID控制器實現(xiàn)的全狀態(tài)跟蹤制導方法。利用準平衡滑翔條件推導了高度、速度及航程等關鍵參數(shù)之間的解析關系,基于此條件結合飛行器當前狀態(tài)與終端約束實現(xiàn)了物理可實現(xiàn)的滑翔軌跡快速規(guī)劃;根據(jù)需要的速度和高度反饋量設計了PID控制器,實現(xiàn)縱向軌跡跟蹤,通過飛行器航向誤差走廊保證了飛行航向。仿真算例驗證了該方法能實現(xiàn)軌跡在線規(guī)劃,并對外部偏差具有較強的魯棒性。
[Abstract]:An online trajectory planning method based on quasi-equilibrium glide condition and a full-state tracking guidance method based on PID controller are proposed for the on-line trajectory planning of aircraft. The analytical relations among the key parameters such as altitude, speed and range are derived by using quasi-equilibrium gliding condition. Based on this condition, the physical and feasible rapid planning of gliding trajectory is realized by combining the current state and terminal constraints of the aircraft. The PID controller is designed according to the required speed and altitude feedback to realize longitudinal trajectory tracking. The flight course is ensured by the flight path error corridor. The simulation results show that the proposed method is robust to the external deviations.
【作者單位】： 國防科學技術大學航天科學與工程學院;空間物理重點實驗室;
【分類號】：V448
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本文編號：1846823