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Control Barrier Function Based Nonlinear Controller for Automatic Carrier Landing

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 novel control barrier function(CBF) based output constraints path following control method, which is applied to automatic carrier landing system. The 6 degrees-of-freedom of aircraft model is converted to an affine model. Based on the transformed affine model, backstepping is used as the main control frame. In order to meet the demand of output constraints, a novel controller based on CBF is designed to constrian path following error. Due to automatic carrier landing system's relative-degree is 4, the exponential control barrier function(ECBF) which constrian path following error is adopted. The stability of the designed controller is verified by Lyapunov analysis. Simulation results show that the error requirement for path following in the final approach can be achieved, so the controller we designed has good path following performance.

源语言英语
主期刊名16th IEEE International Conference on Control, Automation, Robotics and Vision, ICARCV 2020
出版商Institute of Electrical and Electronics Engineers Inc.
584-589
页数6
ISBN(电子版)9781728177090
DOI
出版状态已出版 - 13 12月 2020
活动16th IEEE International Conference on Control, Automation, Robotics and Vision, ICARCV 2020 - Virtual, Shenzhen, 中国
期限: 13 12月 202015 12月 2020

出版系列

姓名16th IEEE International Conference on Control, Automation, Robotics and Vision, ICARCV 2020

会议

会议16th IEEE International Conference on Control, Automation, Robotics and Vision, ICARCV 2020
国家/地区中国
Virtual, Shenzhen
时期13/12/2015/12/20

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