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Active control technology development at NASAIt is noted that the large space systems deployable by means of the Space Shuttle will have increased flexibility, and therefore unprecedented interaction between control and other subsystems. Open loop performance in such systems would be grossly inadequate, prompting active control method development to achieve the required performance levels. The structures in question encompass those of projected science and communications platforms, interplanetary space transportation systems, and manned permanent space stations.
Document ID
19850040435
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dahlgren, J. B.
(NASA Office of Aeronautics and Space Technology Washington, DC, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1983
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
85A22586
Distribution Limits
Public
Copyright
Other

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