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The Magsat three axis arc second precision attitude transfer systemThe Magsat Attitude Transfer System (ATS), which provides attitude alteration in pitch, yaw, and roll is described. A remote vector magnetometer extends from Magsat on a 20 ft boom, requiring vector orientation by reference to coordinate axes determined by a set of star mapping cameras. The ATS was designed to perform in a solar illuminated environment by using an optically narrow bandwidth with synchronous demodulation at 9300 A. The pitch/yaw optical design, the electrooptics, and signal and switching diagrams are provided. Simple mirrors with no moving parts are placed on the magnetometer to reflect a collimated beam from the ATS for attitude indication, which is accurate to one part in 96. Alignment was completed within 24 hr after launch.
Document ID
19820030914
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Schenkel, F. W.
(Johns Hopkins Univ. Laurel, MD, United States)
Heins, R. J.
(Johns Hopkins University Laurel, MD, United States)
Date Acquired
August 10, 2013
Publication Date
December 1, 1981
Publication Information
Publication: vol. 34
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
82A14449
Funding Number(s)
CONTRACT_GRANT: NASA TASK I
CONTRACT_GRANT: N00024-78-C-5384
Distribution Limits
Public
Copyright
Other

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