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Effects of nonlinear damping in flexible space structuresThe classical Krylov-Bogoliubov "averaging" technique is used to study a class of nonlinear damping models, for which the damping force is proportional to the product of positive integer or fractional power of absolute values of displacement and that of velocity. The results are compared with linear viscous damping models. The amplitude decrement of free vibration for a single mode system with nonlinear models depends not only on damping ratio, but also on the initial amplitude, the time to measure the response, frequency of the system, and the powers of displacement and velocity. For the distributed system, the action of nonlinear damping is found to reduce energy of the system as well as to pass energy to higher modes. Experimental evidence such as in Spacecraft Control Laboratory Experiment seems to support the need for nonlinear models.
Document ID
19880062942
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hu, Anren
(DYNACS Engineering Co., Inc. Clearwater, FL, United States)
Taylor, Lawrence W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 88-4059
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference
Location: Minneapolis, MN
Country: United States
Start Date: August 15, 1988
End Date: August 17, 1988
Sponsors: AIAA Guidance
Accession Number
88A50169
Distribution Limits
Public
Copyright
Other

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