文章基本信息

标题：Semidefinite Programming Solution to the Spacecraft Analysis and Control Problem
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作者：Aurélio T. Salton ; Rafael S. Castro ; Bernardo S. Borges 等
期刊名称：IFAC PapersOnLine
印刷版ISSN：2405-8963
出版年度：2017
卷号：50
期号：1
页码：3959-3964
DOI：10.1016/j.ifacol.2017.08.603
语种：English
出版社：Elsevier
摘要：AbstractThis paper provides a semidefinite optimization solution to the analysis and control of a rigid rotating spacecraft. Due to the quaternion representation of a rotating body, the nonlinearities that describe the system are polynomial in nature and may be expressed in the Differential Algebraic Representation (DAR). Once the system is in this form, it is possible to apply linear-based tools for the analysis and control design of the closed loop dynamics. The task is then reduced to that of a semidefinite optimization problem subject to constraints in the form of Linear Matrix Inequalities (LMIs).
关键词：KeywordsDifferential Algebraic RepresentationNonlinear SystemsRigid Spacecraft