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The Method of Averaging for Euler's Equations of Rigid Body Motion

dc.contributor.authorCoppola, Vincent T.en_US
dc.date.accessioned2006-09-08T21:18:46Z
dc.date.available2006-09-08T21:18:46Z
dc.date.issued1997-12en_US
dc.identifier.citationCoppola, Vincent T.; (1997). "The Method of Averaging for Euler's Equations of Rigid Body Motion." Nonlinear Dynamics 14(4): 295-308. <http://hdl.handle.net/2027.42/43321>en_US
dc.identifier.issn0924-090Xen_US
dc.identifier.issn1573-269Xen_US
dc.identifier.urihttps://hdl.handle.net/2027.42/43321
dc.description.abstractWe formulate the method of averaging for perturbations of Euler's equations of rotational motion. Euler's equations are three strongly nonlinear coupled differential equations that can be viewed as a three dimensional oscillator. The method of averaging is used to determine the long-term influence of perturbation terms on the motion by averaging about the nominal rigid body motion. The treatment is applicable to a large class of motions including precession with large nutation – it is not restricted to small motions about simple spins or nearly axi-symmetric bodies. Three examples are shown that demonstrate the accuracy of the method's predictions.en_US
dc.format.extent260649 bytes
dc.format.extent3115 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.language.isoen_US
dc.publisherKluwer Academic Publishers; Springer Science+Business Mediaen_US
dc.subject.otherMethod of Averagingen_US
dc.subject.otherVibration, Dynamical Systems, Controlen_US
dc.subject.otherEngineeringen_US
dc.subject.otherMechanicsen_US
dc.subject.otherMechanical Engineeringen_US
dc.subject.otherAutomotive and Aerospace Engineering, Trafficen_US
dc.subject.otherSpacecraft Attitude Motionen_US
dc.subject.otherElliptic Functionsen_US
dc.titleThe Method of Averaging for Euler's Equations of Rigid Body Motionen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelMathematicsen_US
dc.subject.hlbtoplevelScienceen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumAerospace Engineering Department, University of Michigan, 3041 FXB Bldg., [Ann Arbor, MI, 48109-2118, U.S.Aen_US
dc.contributor.affiliationumcampusAnn Arboren_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/43321/1/11071_2004_Article_140889.pdfen_US
dc.identifier.doihttp://dx.doi.org/10.1023/A:1008215327247en_US
dc.identifier.sourceNonlinear Dynamicsen_US
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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