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Spacecraft control research at NASAFuture missions is space will require controlling spacecraft which are both large and flexible. The limited inherent damping and the uncertain and changing dynamic characteristics of many of these vehicles, such as manned space stations and large antennas, will revolutionize spacecraft control requirements. In preparation for the time that such control systems are required, considerable research and technology development is necessary. A program is in place at NASA for the development of active control technology to support major initiatives for space station and advanced spacecraft. A number of key control technology program needs are cited in the paper as required for these and other future NASA missions together with an integrated controls/structures technology flight experiment to demonstrate and validate technology for large flexible structures.
Document ID
19840016536
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dahlgren, J. B.
(NASA Headquarters Washington, DC United States)
Taylor, L. W., Jr.
(NASA Langley Research Center)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Publication Information
Publication: AGARD Guidance and Control Tech. for Advan. Space Vehicles
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
84N24604
Distribution Limits
Public
Copyright
Other
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