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Robust fuel- and time-optimal control of uncertain flexible space structuresThe problem of computing open-loop, fuel- and time-optimal control inputs for flexible space structures in the face of modeling uncertainty is investigated. Robustified, fuel- and time-optimal pulse sequences are obtained by solving a constrained optimization problem subject to robustness constraints. It is shown that 'bang-off-bang' pulse sequences with a finite number of switchings provide a practical tradeoff among the maneuvering time, fuel consumption, and performance robustness of uncertain flexible space structures.
Document ID
19930067399
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wie, Bong
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Sinha, Ravi
(Arizona State Univ. Tempe, United States)
Sunkel, John
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Cox, Ken
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Guidance, Navigation and Control Conference, Monterey, CA, Aug. 9-11, 1993, Technical Papers. Pt. 2 (A93-51301 22-63)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 93-3804
Accession Number
93A51396
Distribution Limits
Public
Copyright
Other

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