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Simulating Flexible-Spacecraft Dynamics and ControlVersatile program applies to many types of spacecraft and dynamical problems. Flexible Spacecraft Dynamics and Control program (FSD) developed to aid in simulation of large class of flexible and rigid spacecraft. Extremely versatile and used in attitude dynamics and control analysis as well as in-orbit support of deployment and control of spacecraft. Applicable to inertially oriented spinning, Earth-oriented, or gravity-gradient-stabilized spacecraft. Written in FORTRAN 77.
Document ID
19870000188
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Fedor, Joseph
(AVCO Corp.)
Date Acquired
August 13, 2013
Publication Date
April 1, 1987
Publication Information
Publication: NASA Tech Briefs
Volume: 11
Issue: 4
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
GSC-13006
Accession Number
87B10188
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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