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Autonomous attitude determination systemsA summary of autonomous attitude determination systems is presented by separating it into four areas: types of attitude determination systems which can be automated, a description of the attitude determination problem and its solution, specific types of sensors, and the processor requirements of two automated systems. The sensors used in attitude determination have been characteristically carried on-board the spacecraft in the past, so the major development requirement of automated systems is in the area of on-board processors. It is concluded that standardization of computers is not as beneficial as the standardization of computer architecture and the basic components which go into making them. It is also concluded that charge-coupled devices (CCD) or other solid state star tracking devices offer considerable advantages over the image-dissector type of star tracker.
Document ID
19790060401
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Lowrie, J. W.
(Martin Marietta Aerospace Denver, Colo., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AAS 79-005
Meeting Information
Meeting: Guidance and control 1979
Location: Keystone, CO
Start Date: February 24, 1979
End Date: February 28, 1979
Accession Number
79A44414
Funding Number(s)
CONTRACT_GRANT: NASW-3106
Distribution Limits
Public
Copyright
Other

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