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ATLAS solar pointing operationsThe ATLAS-series of Spacelab missions are comprised of a diverse group of scientific instruments including instruments for studying the sun and how the sun's energy changes across an eleven-year solar cycle. The ATLAS solar instruments are located on one or more pallets in the Orbiter payload bay and use the Orbiter as a pointing platform for their examinations of the sun. One of the ATLAS instruments contained a sun sensor which allowed scientists and engineers on the ground to see the pointing error of the sun with respect to the instrument and correct for the error based upon the information coming from the ATLAS 1 and ATLAS 2 missions with particular attention given to identifying the sources of pointing discrepancies of the solar instruments and to describe the crew and ground controller procedures that were developed to correct for these discrepancies. The Orbiter pointing behavior from the ATLAS 1 and ATLAS 2 flights presented in this paper can be applied to future flights which use the Orbiter as a pointing platform.
Document ID
19940031119
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tyler, C. A.
(Teledyne Brown Engineering Huntsville, AL., United States)
Zimmerman, C. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1994
Publication Information
Publication: NASA. Goddard Space Flight Center, Flight Mechanics(Estimation Theory Symposium, 1994
Subject Category
Astronautics (General)
Accession Number
94N35626
Funding Number(s)
CONTRACT_GRANT: NAS8-41000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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