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Interaction of the Space Shuttle on-orbit autopilot with tether dynamicsThe effect of Orbiter flight control on tether dynamics is studied by simulation. Open-loop effects of Orbiter jet firing on tether dynamics are shown, and the potential for closed-loop interaction between tether dynamics and Orbiter flight control is determined. The significance of these effects on Orbiter flight control and tether control is assessed.
Document ID
19890055970
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bergmann, Edward V. (Charles Stark Draper Laboratory, Inc. Cambridge, MA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Intl. Conference on Space Tethers for Science in the Space Station Era
Location: Venice
Country: Italy
Start Date: October 4, 1987
End Date: October 8, 1987
Accession Number
89A43341
Funding Number(s)
CONTRACT_GRANT: NAS8-36602
Distribution Limits
Public
Copyright
Other

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