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Dynamic analysis of an unrestrained, rotating structure through nonlinear simulationAn alternate derivation based on Hamilton's principle of equations of motion of a flexible body for use in nonlinear simulation modeling is presented. The equations include terms representing variation in the inertial properties of the body resulting from flexibility as well as terms coupling rigid body and flexible momenta that arise from satisfaction of only the linear part of the mean axis conditions. An approximate method for including the centrifugal stiffening in a way that permits a variable spin vector is given. The equations are exercised in a simulation program on an example structure initially spinning about its unstable principal axis in a gravity-free vacuum.
Document ID
19880044968
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zeiler, Thomas A.
(PRC Kentron, Inc. Aerospace Technologies Div., Hampton, VA, United States)
Buttrill, Carey S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Cybernetics
Report/Patent Number
AIAA PAPER 88-2232
Report Number: AIAA PAPER 88-2232
Meeting Information
Meeting: Structures, Structural Dynamics and Materials Conference
Location: Williamsburg, VA
Country: United States
Start Date: April 18, 1988
End Date: April 20, 1988
Sponsors: Structures
Accession Number
88A32195
Distribution Limits
Public
Copyright
Other

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