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2012 | OriginalPaper | Chapter

218. LPV Modeling of the Missile Attitude Control System Based on Small Deviation Equation

Authors : Shaobo Ni, Jianwu Wu, Jiayuan Shan, Lei Liu, Yongji Wang, Kun Hu

Published in: Electrical, Information Engineering and Mechatronics 2011

Publisher: Springer London

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Abstract

With a concern about the missile attitude control system, this paper attempts to solve the online calculation method of the coefficient of the small deviation equation, on which a LFT-based LPV model of the missile attitude control system is set up.

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Title: LPV Modeling of the Missile Attitude Control System Based on Small Deviation Equation
Authors: Shaobo Ni
Jianwu Wu
Jiayuan Shan
Lei Liu
Yongji Wang
Kun Hu
Publisher: Springer London
Book: Electrical, Information Engineering and Mechatronics 2011
Print ISBN: 978-1-4471-2466-5

Electronic ISBN: 978-1-4471-2467-2

Copyright Year: 2012
DOI: https://doi.org/10.1007/978-1-4471-2467-2_218