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Active rejection of persistent disturbances in flexible space structuresA dynamic compensator for active rejection of persistent disturbances in flexible space structures is designed on the principle of the H(infinity)-optimization of the sensitivity transfer function matrix. A general state space solution is formulated to the multiinput multioutput H(infinity)-optimal control problem, allowing the use of the H(infinity)-optimal synthesis algorithm for the state-space models of space structures that result from model order reduction. Disturbances encountered in flexible space structures, such as shuttle docking, are investigated using the high-mode and the reduced-order models of a cantilevered two-bay truss, demonstrating the applicability of the H(infinity)-optimal approach.
Document ID
19900060627
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hwang, Cheng-Neng
(Texas A&M Univ. College Station, TX, United States)
Jayasuriya, Suhada
(Texas A&M Univ. College Station, TX, United States)
Parlos, Alexander G.
(Texas A & M University College Station, United States)
Sunkel, John W.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 90-3428
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference
Location: Portland, OR
Country: United States
Start Date: August 20, 1990
End Date: August 22, 1990
Accession Number
90A47682
Funding Number(s)
CONTRACT_GRANT: NAG9-347
Distribution Limits
Public
Copyright
Other

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