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Hybrid equations of motion for flexible multibody systems using quasi-coordinatesA variety of engineering systems, such as automobiles, aircraft, rotorcraft, robots, spacecraft, etc., can be modeled as flexible multibody systems. The individual flexible bodies are in general characterized by distributed parameters. In most earlier investigations they were approximated by some spatial discretization procedure, such as the classical Rayleigh-Ritz method or the finite element method. This paper presents a mathematical formulation for distributed-parameter multibody systems consisting of a set of hybrid (ordinary and partial) differential equations of motion in terms of quasi-coordinates. Moreover, the equations for the elastic motions include rotatory inertia and shear deformation effects. The hybrid set is cast in state form, thus making it suitable for control design.
Document ID
19930067365
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Meirovitch, L.
(NASA Langley Research Center Hampton, VA, United States)
Stemple, T.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Guidance, Navigation and Control Conference, Monterey, CA, Aug. 9-11, 1993, Technical Papers. Pt. 2 (A93-51301 22-63)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Cybernetics
Report/Patent Number
AIAA PAPER 93-3767
Accession Number
93A51362
Funding Number(s)
CONTRACT_GRANT: F49620-89-C-0045
CONTRACT_GRANT: NAG1-225
Distribution Limits
Public
Copyright
Other

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