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無人直升機自抗擾自適應軌跡跟蹤混合控制

姜辰 王浩文 李健珂 李亮君

姜辰, 王浩文, 李健珂, 李亮君. 無人直升機自抗擾自適應軌跡跟蹤混合控制[J]. 工程科學學報, 2017, 39(11): 1743-1752. doi: 10.13374/j.issn2095-9389.2017.11.018
引用本文: 姜辰, 王浩文, 李健珂, 李亮君. 無人直升機自抗擾自適應軌跡跟蹤混合控制[J]. 工程科學學報, 2017, 39(11): 1743-1752. doi: 10.13374/j.issn2095-9389.2017.11.018
JIANG Chen, WANG Hao-wen, LI Jian-ke, LI Liang-jun. Trajectory-tracking hybrid controller based on ADRC and adaptive control for unmanned helicopters[J]. Chinese Journal of Engineering, 2017, 39(11): 1743-1752. doi: 10.13374/j.issn2095-9389.2017.11.018
Citation: JIANG Chen, WANG Hao-wen, LI Jian-ke, LI Liang-jun. Trajectory-tracking hybrid controller based on ADRC and adaptive control for unmanned helicopters[J]. Chinese Journal of Engineering, 2017, 39(11): 1743-1752. doi: 10.13374/j.issn2095-9389.2017.11.018

無人直升機自抗擾自適應軌跡跟蹤混合控制

doi: 10.13374/j.issn2095-9389.2017.11.018
詳細信息
  • 中圖分類號: V249.1

Trajectory-tracking hybrid controller based on ADRC and adaptive control for unmanned helicopters

  • 摘要: 為滿足無人直升機高精度軌跡跟蹤的控制需求,并降低直升機動力學模型誤差對飛行控制器飛行控制效果產生的影響,提出自抗擾自適應直升機混合控制.該控制器的內環控制采用模型跟隨自適應控制,通過使用動量反向傳播算法(MOBP)對該內環控制參數進行實時優化.通過使用自抗擾控制(ADRC)對直升機的水平速度進行控制.仿真結果表明,該混合控制器能夠實現直升機對預定軌跡的跟蹤.相對PID和級聯ADRC控制,該控制器具有更好的抗擾性和魯棒性.通過在200 kg級的專業植保無人直升機XV-2上搭載所提出的控制器,使其自主飛行軌跡跟蹤控制的均方根誤差在0.6 m以內.

     

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  • 收稿日期:  2017-01-18

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