跳到主要导航 跳到搜索 跳到主要内容

Output tracking of VTOL aircraft with delayed attitude measurements

  • 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 we consider the flight-trajectory tracking problem of an input-disturbed non-minimum phase vertical takeoff and landing (VTOL) aircraft with delayed attitude measurements. By applying the first-order Padé approximation method to deal with the time delays, the problem is reduced to the output tracking of a new high-order non-minimum phase system without delay, whose dynamics are then separated into minimum-phase and non-minimum-phase parts. By using Devasia's stable noncausal inversion method, the ideal internal states of the non-minimum-phase subsystem are obtained and two error subsystems are ultimately constructed. We propose two low-dimensional sliding mode controllers to stabilize the error subsystems, which can render the overall closed-loop system stable in spite of the existence of disturbances. Simulations are performed to show the main results of this paper.

源语言英语
主期刊名Proceedings of the 48th IEEE Conference on Decision and Control held jointly with 2009 28th Chinese Control Conference, CDC/CCC 2009
出版商Institute of Electrical and Electronics Engineers Inc.
2528-2533
页数6
ISBN(印刷版)9781424438716
DOI
出版状态已出版 - 2009
活动48th IEEE Conference on Decision and Control held jointly with 2009 28th Chinese Control Conference, CDC/CCC 2009 - Shanghai, 中国
期限: 15 12月 200918 12月 2009

出版系列

姓名Proceedings of the IEEE Conference on Decision and Control
ISSN(印刷版)0743-1546
ISSN(电子版)2576-2370

会议

会议48th IEEE Conference on Decision and Control held jointly with 2009 28th Chinese Control Conference, CDC/CCC 2009
国家/地区中国
Shanghai
时期15/12/0918/12/09

学术指纹

探究 'Output tracking of VTOL aircraft with delayed attitude measurements' 的科研主题。它们共同构成独一无二的学术指纹。

引用此