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

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

doi:10.1007/978-1-4471-2467-2_218

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

Shaobo Ni, Yongji Wang + Show 4 more

https://doi.org/10.1007/978-1-4471-2467-2_218

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Publication Date: Jan 1, 2012

Citations: 7

Affiliation: Beijing Institute of Technology, Huazhong University of Science and Technology, Beijing Aerospace Flight Control Center

#Missile Attitude Control System #Missile System + Show 8 more

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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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