Differential flatness based control of Glide-reentry anti-vessel missile engineless part

Proceedings of the 30th Chinese Control Conference, CCC 2011(2011)

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摘要
Nonlinear inverse dynamic controller based on differential flatness was designed for Glide-reentry anti-vessel missile terminal engineless part. Aerodynamic data was processed to make the missile model flat. Brake rudder was introduced to control terminal energy and fulfill the requirement of flatness. © 2011 Chinese Assoc of Automati.
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关键词
anti-vessel missile,differential flatness,glide-reentry,nonlinear inverse dynamic,nonlinear systems,trajectory,atmospheric modeling,vehicle dynamics,aerodynamics
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