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Measurement of the passive attitude control performance of a recovered spacecraftA novel silver detector incorporated in the Long Duration Exposure Facility (LDEF) has been used to measure the attitude stability of the vehicle. It is thereby established that the LDEF spacecraft maintained a very stable attitude during its nearly 6-year-long flight, notwithstanding a small offset yaw of 8.0 +/- 0.4 deg clockwise from nominal attitude (as viewed from space) and a +/- 0.2-deg oscillation about this offset yaw. LDEF experiments which depend on orientation relative to the forward direction may need to be corrected for the angular offset.
Document ID
19920038566
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Gregory, J. C.
(Alabama, University Huntsville, United States)
Peters, P. N.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
February 1, 1992
Publication Information
Publication: Journal of Guidance, Control, and Dynamics
Volume: 15
ISSN: 0731-5090
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
92A21190
Funding Number(s)
CONTRACT_GRANT: NAGW-812
CONTRACT_GRANT: NAS8-36645
Distribution Limits
Public
Copyright
Other

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