Title :
Differential flatness based control of Glide-reentry anti-vessel missile engineless part
Author :
Li Congying ; Han Lei ; Xu Xiaofei ; Yu Jinyong
Author_Institution :
7th Dept., Naval Aeronaut. Eng. Inst., Yantai, China
Abstract :
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.
Keywords :
aerodynamics; control system synthesis; missile control; nonlinear control systems; vehicle dynamics; aerodynamic data; brake rudder; differential flatness based control; glide-reentry antivessel missile engineless part; nonlinear inverse dynamic controller; terminal energy; Aerodynamics; Atmospheric modeling; Conferences; Electronic mail; Missiles; Nonlinear systems; Trajectory; Anti-Vessel Missile; Differential Flatness; Glide-Reentry; Nonlinear Inverse Dynamic;
Conference_Titel :
Control Conference (CCC), 2011 30th Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4577-0677-6
Electronic_ISBN :
1934-1768
