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Optimal Prediction Control Allocation Algorithm for Tiltrotor Aircraft

  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This paper proposes a control framework using optimal prediction control allocation method (PM) and active disturbance rejection controller. First, the PM algorithm is adopted to extend the Attainable Moment Set compared with Pseudo-Inverse method (PI). By compensating the solution with null space vector, the saturation problem is solved while outputting the desired moments. Second, active disturbance rejection controller is adopted to observe and compensate the complex disturbance during the transition of tiltrotor aircraft. Numerical simulations demonstrate that PM can output optimal control allocation solution to generate larger moments under the same desired moments input compared with PI. The 6-DOF flight simulation shows that the overall control frame has better performance.

源语言英语
主期刊名Advances in Guidance, Navigation and Control - Proceedings of 2020 International Conference on Guidance, Navigation and Control, ICGNC 2020
编辑Liang Yan, Haibin Duan, Xiang Yu
出版商Springer Science and Business Media Deutschland GmbH
1183-1193
页数11
ISBN(印刷版)9789811581540
DOI
出版状态已出版 - 2022
活动International Conference on Guidance, Navigation and Control, ICGNC 2020 - Tianjin, 中国
期限: 23 10月 202025 10月 2020

出版系列

姓名Lecture Notes in Electrical Engineering
644 LNEE
ISSN(印刷版)1876-1100
ISSN(电子版)1876-1119

会议

会议International Conference on Guidance, Navigation and Control, ICGNC 2020
国家/地区中国
Tianjin
时期23/10/2025/10/20

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