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Relative motion modeling and control for autonomus UAV carrier landing

  • 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

In this paper, the relative motion model and control strategy for autonomous unmanned aerial vehicle(UAV) carrier landing are addressed. Firstly, a coupled six degrees of freedom(6-DOF) non-linear relative motion model is established from (6-DOF) UAV and carrier models. Then the (6-DOF) relative motion model is simplified to the four degree of freedom (4-DOF) model to facilitate the control design, because of the underactuated characteristic of two vehicles. Secondly, the feedback linearization control law is proposed to control the UAV towards the aircraft carrier with constant forward, vertical velocity and lateral position and yaw angle. Finally, simulation results demonstrate the effectiveness of the proposed control system.

源语言英语
主期刊名Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016
出版商Institute of Electrical and Electronics Engineers Inc.
页6415-6421
页数7
ISBN(电子版)9781467397148
DOI
出版状态已出版 - 3 8月 2016
活动28th Chinese Control and Decision Conference, CCDC 2016 - Yinchuan, 中国
期限: 28 5月 2016 → 30 5月 2016

丛书

姓名Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016

会议

会议28th Chinese Control and Decision Conference, CCDC 2016
国家/地区中国
市Yinchuan
时期28/05/16 → 30/05/16

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