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Design of Flight Control System for Flexible Mars Rotorcraft

  • Wangwang Zhang
  • , Bin Xu*
  • , Yu Zhang
  • , Changle Xiang
  • , Wei Fan
  • , Shouxing Tang
  • *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

The importance of exploring Mars is self-evident, Mars's extremely low atmospheric density, resulting in Mars drones must have enough light weight. Multi-rotor unmanned aerial vehicle (UAV) with flexible racks offer another possibility for the lightweight design of Mars Rotorcraft. Based on the unique atmospheric environment of Mars, a flexible rotorcraft with ultra-light structure is designed in this paper, and the stability control of this flexible UAV is studied. A compound stability augmentation control system is proposed, which adopts PID controller as the main controller and L1 adaptive controller as the composite controller with output feedback to realize the stable flight of flexible Mars UAV. And through the flight experiment, it is proved that the designed controller has a good stability control effect for the flexible Mars UAV.

源语言英语
主期刊名Proceedings of 2023 IEEE International Conference on Unmanned Systems, ICUS 2023
编辑Rong Song
出版商Institute of Electrical and Electronics Engineers Inc.
页546-551
页数6
ISBN(电子版)9798350316308
DOI
出版状态已出版 - 2023
活动2023 IEEE International Conference on Unmanned Systems, ICUS 2023 - Hefei, 中国
期限: 13 10月 2023 → 15 10月 2023

丛书

姓名Proceedings of 2023 IEEE International Conference on Unmanned Systems, ICUS 2023

会议

会议2023 IEEE International Conference on Unmanned Systems, ICUS 2023
国家/地区中国
市Hefei
时期13/10/23 → 15/10/23

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