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Controlled Lagrangians control for a quadrotor helicopter

  • 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

The controller design technique based on Controlled Lagrangians (CL) is presented for a quadrotor helicopter with under-actuation degree 2. Firstly, the dynamic model of the quadrotor used for controller design is introduced, and the model is linearized at its equilibrium. Then, the CL method is used for the linearized system to design its controller and the matching conditions satisfied for the controller are derived. Stability analysis shows that the controlled closed-loop system is asymptotically stable. The proposed method solves the under-actuated problem for quadrotor and avoids the dependence of control law design under the time-scale separation assumption. Finally, simulation results for the quadrotor helicopter to hovering in a certain position are illustrated to verify effectiveness of the proposed method.

源语言英语
主期刊名Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015
出版商Institute of Electrical and Electronics Engineers Inc.
6097-6102
页数6
ISBN(电子版)9781479970179
DOI
出版状态已出版 - 17 7月 2015
活动27th Chinese Control and Decision Conference, CCDC 2015 - Qingdao, 中国
期限: 23 5月 201525 5月 2015

出版系列

姓名Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015

会议

会议27th Chinese Control and Decision Conference, CCDC 2015
国家/地区中国
Qingdao
时期23/05/1525/05/15

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