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

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

Lecture notes in electrical engineering（2012）

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摘要

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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关键词

Missile control,Attitude control,Variable gain control,Linear variable parameter

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