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Application of adaptive control to space stationsThe space station will be deployed and assembled in low earth orbit with multiple Shuttle trips. Several construction phases will be required involving both ground and in-orbit operations. In this paper, the construction process of a four-panel space station and its control problems are discussed. The applicability of a direct model reference adaptive control technique with plant augmentation is investigated. Control during several key assembly operation periods has been simulated. These include Shuttle docking with initial-phase station, habitat module mating, and Shuttle docking with operational station. High rate of convergence and robust performance have been observed for all the simulated cases even with 40 percent model parameter errors and model truncations and more than 100 percent instant mass property variations. Controller with severe gain saturations is also discussed and results show only slight performance deterioration.
Document ID
19850063801
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ih, C.-H. C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wang, S. J.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Leondes, C. T.
(California, University Los Angeles, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 85-1970
Report Number: AIAA PAPER 85-1970
Meeting Information
Meeting: Guidance, Navigation and Control Conference
Location: Snowmass, CO
Start Date: August 19, 1985
End Date: August 21, 1985
Accession Number
85A45952
Distribution Limits
Public
Copyright
Other

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