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A low cost LST pointing control systemVigorous efforts to reduce costs, coupled with changes in LST guidelines, took place in the Fall of 1974. These events made a new design of the LST and its Pointing and Attitude Control System possible. The major design changes are summarized as: an annular Support Systems Module; removal of image motion compensation; reaction wheels instead of CMG's; a magnetic torquer system to also perform the emergency and backup functions, eliminating the previously required mass expulsion system. Preliminary analysis indicates the Low Cost LST concept can meet the newly defined requirements and results in a significantly reduced development cost.
Document ID
19750057556
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Glaese, J. R.
Kennel, H. F.
Nurre, G. S.
Seltzer, S. M.
Shelton, H. L.
(NASA Marshall Space Flight Center Systems Dynamics Laboratory, Huntsville, Ala., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AIAA PAPER 75-1057
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Guidance and Control Conference
Location: Boston, MA
Start Date: August 20, 1975
End Date: August 22, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A41628
Distribution Limits
Public
Copyright
Other

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