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Results of flexible spacecraft attitude control studies utilizing hybrid coordinatesHybrid coordinate formulation for flexible space vehicle attitude control system design
Document ID
19710042210
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Fleischer, G. E.
Likins, P. W.
Date Acquired
August 6, 2013
Publication Date
March 1, 1971
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 70-20
Report Number: AIAA PAPER 70-20
Meeting Information
Meeting: AEROSPACE SCIENCES MEETING
Location: NEW YORK, NY
Start Date: January 19, 1970
End Date: January 21, 1970
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
71A22907
Distribution Limits
Public
Copyright
Other

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