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Use of reduced basis technique in the inverse dynamics of large space cranesThe inverse dynamics of adaptive structures used as space cranes can prove computationally expensive in the case of large structures, due to the large number of degrees of freedom involved. Consequently, reduced basis techniques (reduction techniques) are frequently used to reduce the problem size to a time manageable level (for possible use in real time control). A reduced basis technique is proposed which is different from, but related to, the path-derivatives reduction technique. A linearly independent set of deflection n-tuples is used, chosen at the beginning of the time range in which it is wished to reduce the equations, in whose subspace it is assumed that the deflection vectors of the unreduced problem will lie (approximately).
Document ID
19910058114
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Das, S. K.
(Duke Univ. Durham, NC, United States)
Utku, S.
(Duke University Durham, NC, United States)
Wada, B. K.
(JPL Pasadena, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Publication Information
Publication: Computing Systems in Engineering
Volume: 1
Issue: 4-Feb
ISSN: 0956-0521
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91A42737
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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