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Active Disturbance Rejection Altitude Control for a QuadPlane

  • Hailong Zhao
  • , Yuanqing Xia*
  • , Dailiang Ma
  • , Chenxi Hao
  • , Feng Yu
  • *此作品的通讯作者
  • Beijing Institute of Technology

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

Quadplane is a hybrid aircraft which combines both quadrotor and traditional fixed-wing aircraft, and is also called fixed-wing vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV). Quadplane keeps the high speed and endurance of fixed-wing UAVs, and has the ability of VTOL hovering as quadrotors. In this paper, a quadplane platform is constructed. Moreover, to improve the altitude control performance during the transition phase between two flight modes, a model-based nonlinear weight assignment principle and an active disturbance rejection control (ADRC) strategy are proposed. Finally, the effectiveness of aerodynamic modelling and controller is verified via simulations.

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
页329-342
页数14
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 2020 → 25 10月 2020

丛书

姓名Lecture Notes in Electrical Engineering
卷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
市Tianjin
时期23/10/20 → 25/10/20

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