The Taylor series method for the problem of the rotational motion of a rigid satellite

DOI10.1007/BF00627552zbMath0835.70003OpenAlexW2093442737WikidataQ96744419 ScholiaQ96744419MaRDI QIDQ1905408

Andrzej J. Maciejewski, Krzysztof Goździewski

Publication date: 10 January 1996

Published in: Astrophysics and Space Science (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00627552

zbMATH Keywords

integration of differential equations

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Free motion of a rigid body (70E15) Orbital mechanics (70M20)

Cites Work

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• Integrators for Lie-Poisson dynamical systems
• Solutions homoclinic to regular precessions of a symmetric satellite
• Symplectic integration of Hamiltonian systems
• Solving Ordinary Differential Equations Using Taylor Series
• Studies in the application of recurrence relations to special perturbation methods
• Numerical integration of differential equations in the presence of first integrals: observer method
• Solution of theN-body problem with recurrent power series
• Practical considerations in the numerical solution of theN-body problem by Taylor series methods