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Impact of space station appendage vibrations on the pointing performance of gimballed payloadsA study of the interface problems between the Space Station Structure (vibrations) and the Payload Pointing Control System was undertaken. A major goal of the study was to identify any bounding factors that might limit the achievement of required pointing accuracies. A major result is that the space station will have a disturbance-rich environment and the background levels will be large enough to impact the pointing of some of the payloads. The need for an interface vibration specification between the structure and the payloads was identified.
Document ID
19870013300
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hughes, Robert O.
(General Electric Co. Philadelphia, PA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Publication Information
Publication: NASA. Marshall Space Flight Center Structural Dynamics and Control Interaction of Flexible Structures 841-866 (SEE N87-22729 16-15)
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N22733
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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