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Satellite attitude control using a torqued, 2-axis-gimbaled boom as the actuator.Torqued two axis gimbaled boom actuator satellite attitude control
Document ID
19690065256
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Buckingham, A. G.
Gatlin, J. A.
Pleasants, W. H.
Date Acquired
August 5, 2013
Publication Date
September 1, 1969
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 68-857
Report Number: AIAA PAPER 68-857
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, GUIDANCE, CONTROL, AND FLIGHT DYNAMICS CONFERENCE
Location: PASADENA, CALIF.
Start Date: August 12, 1968
End Date: August 14, 1968
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A43245
Distribution Limits
Public
Copyright
Other

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