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A model for the three-dimensional spacecraft control laboratory experimentA model for the three-dimensional Spacecraft Control Laboratory Experiment (SCOLE) is developed. The objective behind this method of modelling is to utilize the basic partial differential equations of motion for this distributed parameter system and not to use the modal expansion in developing the model. The final model obtained is in terms of a transfer function matrix which relates the flexible mast parameters like displacement, slope, shear stress, etc. to external forces and moments.
Document ID
19910013038
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kakad, Yogendra P. (North Carolina Univ. Charlotte, NC, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1991
Publication Information
Publication: NASA. Langley Research Center, Fourth NASA Workshop on Computational Control of Flexible Aerospace Systems, Part 2
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91N22351
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19910013018Collected WorksFourth NASA Workshop on Computational Control of Flexible Aerospace Systems, part 2
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