文章基本信息

标题：Design and Analysis of Nonlinear Constrained Control Algorithm for Rigid Aircraft ⁎
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作者：Bo Yu ; HaiBo Du ; Jun Zhou 等
期刊名称：IFAC PapersOnLine
印刷版ISSN：2405-8963
出版年度：2020
卷号：53
期号：5
页码：476-478
DOI：10.1016/j.ifacol.2021.04.132
语种：English
出版社：Elsevier
摘要：AbstractIn this paper, a method to the problem of the attitude stabilization control for the rigid aircraft under angular velocity constrains is presented. Firstly, a finite-time controller with time-vary state-dependent gains is proposed. Then, based on the homogeneous theory, demonstrates the rigid body spacecraft with angular velocity constrains can be stabilized in a finite time. At the end, the effectiveness and validity of the developed method is verified by numerical simulation.
关键词：Keywordsattitude controlangular velocity constraintfinite-time