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

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4 Author(s)
Congying Li ; 7th Department of Naval Aeronautical Engineering Institute, Yantai 264001, China ; Lei Han ; Xiaofei Xu ; Jinyong Yu

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.

Published in:

Control Conference (CCC), 2011 30th Chinese

Date of Conference:

22-24 July 2011