DocumentCode :
2618786
Title :
Design of Variable Structure Stability Control Loop for Anti-air Missile with Swing Nozzle Thrust Vector Control
Author :
Xiaofeng, Zhang ; Xiaoping, Zhu ; Jun, Yang
Author_Institution :
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´´an, China
Volume :
1
fYear :
2011
fDate :
6-7 Jan. 2011
Firstpage :
1014
Lastpage :
1017
Abstract :
A new design method of stability control loop for the swing nozzle thrust control anti-air missile is present in this paper. Firstly, the model of the missile which considered the aeroservoelastic and swing nozzle effect is given. Then, based on the small error linearization model, the theory of Variable Structure Control is used for stability control loop design for the missile with the model uncertainty and disturbance, the framework of the Variable Structure Control of the longitude autopilot is constructed. Finally, the simulation on the control system shows that the robust stability and performance is achieved.
Keywords :
linearisation techniques; missile control; nozzles; robust control; variable structure systems; aeroservoelastic; anti-air missile; control system; linearization model; model uncertainty; robust control; stability control loop; swing nozzle thrust vector control; variable structure control; Acceleration; Aerodynamics; Atmospheric modeling; Control systems; Mathematical model; Missiles; Stability analysis; Aeroservoelastic; Robust performance; Swing Nozzle Thrust Vector Control; Variable Structure Control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Measuring Technology and Mechatronics Automation (ICMTMA), 2011 Third International Conference on
Conference_Location :
Shangshai
Print_ISBN :
978-1-4244-9010-3
Type :
conf
DOI :
10.1109/ICMTMA.2011.254
Filename :
5720957
Link To Document :
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