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On-orbit parameter and disturbance identification for Space StationThis paper describes recent efforts directed at the problem of on-orbit parameter and disturbance identification for the Space Station. Techniques are developed for identification of rigid body parameters, flexible body parameters, and quasi-static disturbances relevant to the Power Tower configuration currently under investigation by NASA. The paper concludes with a case study investigating the identification of modal frequencies in a 15 degree of freedom planar model of the Space Station under a variety of operational settings.
Document ID
19860054739
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bayard, D. S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hadaegh, F. Y.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ih, C. C.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
86A39477
Distribution Limits
Public
Copyright
Other

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