DocumentCode
1794962
Title
Design of servo system robust controller for multiple launcher
Author
Changjun Xia ; Jinguo Tang ; Changjin Wang
Author_Institution
Dept. of Airborne Vehicle Eng., Naval Aeronaut. & Astronaut. Univ.(NAAU), Yantai, China
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
845
Lastpage
849
Abstract
This paper designs a robust controller to ensure that the control tracking performance of the multiple launcher servo system maintain robustness under the influence of the parameter perturbation and uncertain disturbance. First the system differential dynamic model with parameter perturbation and disturbance is established, state equation of error between the reference model and the system is deduced. Second, robust controller is designed according to the system error, the robust control system is proved to be global stable by Lyapunov theorem. Last, the paper makes simulation, the simulation result of robust controller is compared with that of PID controller, and comparison shows robust controller has better robustness than PID controller for multiple launcher servo system.
Keywords
Lyapunov methods; aerospace control; control system synthesis; robust control; servomechanisms; three-term control; Lyapunov theorem; PID controller; control tracking performance; global stable; multiple launcher servo system; parameter disturbance; parameter perturbation; reference model; robust control system; servo system robust controller design; state equation; system differential dynamic model; system error; Equations; Load modeling; Mathematical model; Missiles; Robust control; Robustness; Servomotors;
fLanguage
English
Publisher
ieee
Conference_Titel
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location
Yantai
Print_ISBN
978-1-4799-4700-3
Type
conf
DOI
10.1109/CGNCC.2014.7007319
Filename
7007319
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