DocumentCode :
1929897
Title :
Researching variable structure control of moving mass reentry-vehicles
Author :
Lin, Peng ; Zhou, Jun
Author_Institution :
Inst. of Precision Guidance & Control, Northwestern Polytech. Univ., Xi´´an, China
Volume :
8
fYear :
2010
fDate :
9-11 July 2010
Firstpage :
126
Lastpage :
129
Abstract :
This paper deals with the control of an axisymmetric moving mass actuated reentry vehicle. Three channel stable dynamic equations of the reentry vehicle are obtained derived from Newtonian theory. Since the maneuvering flighting in the reentry stage is mainly in the longitudinal plane, linear equations of the vehicle in the longitudinal plane based on linear perturbation theory are available. In addition, the control system of the moving mass actuated reentry vehicle is designed based on variable structure control method. Results obtained from simulations indicate the nonlinear model satisfy performance index demands of the attitude control.
Keywords :
Newton method; attitude control; nonlinear control systems; perturbation techniques; variable structure systems; vehicles; Newtonian theory; attitude control; axisymmetric moving mass actuated reentry vehicle; channel stable dynamic equations; linear perturbation theory; nonlinear model; variable structure control; Attitude control; attitude control; model-reference variable structure control; moving mass control; reentry vehicle;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Science and Information Technology (ICCSIT), 2010 3rd IEEE International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4244-5537-9
Type :
conf
DOI :
10.1109/ICCSIT.2010.5563654
Filename :
5563654
Link To Document :
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