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Application of control moment gyros in the attitude control of the Apollo Telescope Mount.Control moment gyro subsystem application in attitude control system of Apollo Telescope Mount for solar phenomena data acquisition
Document ID
19680056593
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chubb, W. B.
Epstein, M.
Date Acquired
August 4, 2013
Publication Date
August 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 68-866
Report Number: AIAA PAPER 68-866
Meeting Information
Meeting: GUIDANCE, CONTROL, AND FLIGHT DYNAMICS CONFERENCE
Location: PASADENA, CA
Start Date: August 12, 1968
End Date: August 14, 1968
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A37565
Distribution Limits
Public
Copyright
Other

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