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Sliding Mode Control of the X-33 Vehicle in Launch ModeThe "nested" structure of the control system for the X33 vehicle in launch mode is developed. Employing backstopping concepts, 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.
Document ID
19990084057
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Shtessel, Yuri (Alabama Univ. Huntsville, AL United States)
Jackson, Mark (NASA Marshall Space Flight Center Huntsville, AL United States)
Hall, Charles (NASA Marshall Space Flight Center Huntsville, AL United States)
Krupp, Don (NASA Marshall Space Flight Center Huntsville, AL United States)
Hendrix, N. Douglas (NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1998
Subject Category
Launch Vehicles And Space Vehicles
Distribution Limits
Public
Copyright
Other

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