DocumentCode
3504610
Title
Sliding mode control of the X33 vehicle in launch mode
Author
Shtessel, Yuri ; Jackson, Mark ; Hall, Charles ; Krupp, Don ; Hendrix, N. Douglas
Author_Institution
Dept. of Electr. & Comput. Eng., Alabama Univ., Huntsville, AL, USA
Volume
2
fYear
1998
fDate
21-26 Jun 1998
Firstpage
1143
Abstract
The “nested” structure of the control system for the X33 vehicle in launch mode is developed. The outer loop (guidance) and the inner loop (rates) continuous sliding mode controllers are designed. Simulations of the 3-DOF model of the X33 launch vehicle showed an accurate, robust, de-coupled tracking performance
Keywords
attitude control; control system synthesis; nonlinear control systems; robust control; space vehicles; tracking; variable structure systems; 3-DOF model; X33 launch vehicle; attitude control; flight control; guidance; inner loop; nonlinear control systems; outer loop; robust control; sliding mode control; tracking; Actuators; Control systems; Fuels; Motion control; Nonlinear control systems; Nonlinear equations; Robust control; Sliding mode control; Stability; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1998. Proceedings of the 1998
Conference_Location
Philadelphia, PA
ISSN
0743-1619
Print_ISBN
0-7803-4530-4
Type
conf
DOI
10.1109/ACC.1998.703590
Filename
703590
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