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Refinements on the pinhole camera measurements of the LDEF attitudeThe results from the University of Alabama in Huntsville (UAH) pinhole camera were reanalyzed to include the effects of corotation of the atmosphere with the Earth as well as satellite oscillation. Previous results from the instrument showed that the satellite had stable attitude offsets in yaw of 8.0 deg and 1.0 deg in pitch; these offsets are unchanged by the present analysis. The primary impact zone of oxygen, i.e., the directly exposed spot on a silver detector, had a ratio of major to minor axes equal to 1.05, which was interpreted as being caused by a small oscillation of plus or minus 0.35 degrees (with precision plus or minus 0.15 degrees). The present analysis shows that the observed effect can largely be accounted for by atmospheric corotation, but that an additional oscillation in yaw of the order of a degree cannot be excluded. The sensitivity of the pinhole camera to satellite oscillations is shown to decrease nonlinearly with decreasing magnitude of the oscillation and to vary inversely with the gas temperature.
Document ID
19930020433
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Peters, Palmer N.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Whitehouse, Paul N.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Gregory, John C.
(Alabama Univ. Huntsville., United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1993
Publication Information
Publication: NASA. Langley Research Center, LDEF: 69 Months in Space. Part 1: Second Post-Retrieval Symposium
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93N29622
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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