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The Method of Averaging for Euler's Equations of Rigid Body Motion
Authors:Coppola  Vincent T.
Affiliation:(1) Aerospace Engineering Department, University of Michigan, 3041 FXB Bldg., [Ann Arbor, MI, 48109-2118, U.S.A
Abstract:We 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.
Keywords:Spacecraft attitude motion  method of averaging  elliptic functions
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