A normalized form of Euler’s equations is rewritten in a variation of parameters approach using amplitudes and angular displacement as parameters. This new form is compact and yields a more accurate numerically integrated solution over longer simulation times than does a conventional integration of the Euler equations.
Issue Section:
Brief Notes
1.
Bond
V. R.
1996
, “A Variation of Parameters Approach for the Solution of the Differential Equations for the Rotational Motion of a Rigid Body
,” Proceedings of the 6th AAS/AIAA Spaceflight Mechanics Meeting: Advances in the Astronautical Sciences
, Vol. 93
, Part II, p. 1113
1113
, abstract (full paper not published).2.
Donaldson
J. D.
Jezewski
D. J.
1977
, “An Element Formulation for Perturbed Motion About the Center of Mass
,” Celestial Mechanics
, Vol. 16
, pp. 367
–387
.3.
Kraige
G. L.
Junkins
J. L.
1976
, “Perturbation Formulations for Satellite Attitude Dynamics
,” Celestial Mechanics
, Vol. 13
, pp. 39
–64
.4.
Kraige
G. L.
Skaar
S. B.
1977
, “A Variation of Parameters Approach to the Arbitrarily Torqued, Asymmetric Rigid Body Problem
,” Journal of the Astronautical Sciences
, Vol. 25
, pp. 207
–226
.5.
Kraige, G. L., 1978, “The Development and Numerical Testing of a Variation of Parameters Approach to the Arbitrarily Torqued, Asymmetric Rigid Body Problem,” Report No. VP1-E-78-9, Virginia Polytechnic Institute, Blacksburg, VA, pp. 1–85.
6.
Richardson
D. L.
Schmidt
D.
Mitchell
J. W.
1998
, “Improved Chebyshev Methods for the Numerical Integration of First-Order Differential Equations
,” Proceedings of the 8th AAS/AIAA Spaceflight Mechanics Meeting: Advances in the Astronautical Sciences
, Vol. 99
, Part II, pp. 1533
–1544
.7.
Williams
T.
Tanygin
S.
1996
, “Dynamics of a Near-Symmetrical Spacecraft Driven by a Constant Thrust
,” Proceedings of the 6th AAS/AIAA Spaceflight Mechanics Meeting: Advances in the Astronautical Sciences
, Vol. 93
, Part II, pp. 925
–944
.
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