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An advanced tracker design for pointing and control of space vehicles using the charge injection deviceThe use of charge transfer devices (CTD) in pointing and control of space vehicles is examined, with emphasis on the use of charge injection devices (CID). The selection of CTD type and CID operation, including CID signal and noise analysis and signal improvement, are discussed. Star tracking operational advantages of the CTD are pointed out, and the tracking optical concept is discussed and graphically depicted. The position interpolation procedure and the effects of rate of stellar motion on position interpolation are considered, and error analysis is examined. Finally, the breadboard and test program are discussed in detail, coarse and fine acquisition, test for star, track pattern, test procedure and results. An overall accuracy performance of approximately 0.02 pixels or approximately 0.8 arcsec for the test equipment and tracker was obtained.
Document ID
19820062082
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Jones, C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Kollodge, J. C.
(Ball Corp. Ball Aerospace Systems Div., Boulder, CO, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AAS 82-031
Meeting Information
Meeting: Guidance and control 1982
Location: Keystone, CO
Country: United States
Start Date: January 30, 1982
End Date: February 3, 1982
Accession Number
82A45617
Funding Number(s)
CONTRACT_GRANT: NAS8-34263
Distribution Limits
Public
Copyright
Other

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