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Motion of a spacecraft with magnetic damper

Motion of spacecraft with magnetic damper

descriptionPublicationkeyboard_double_arrow_right Article , Other literature type 10 Aug 1992Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:Journal of Guidance, Control, and Dynamics, volume 19, pages 980-982 (issn: 0731-5090, eissn: 1533-3884,

Authors: Anren Hu; Carlos M. Roithmayr; Richard Chipman;

doi: 10.2514/3.21732 , 10.2514/6.1992-4367

Motion of a spacecraft with magnetic damper

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Abstract

Two methods of numerically simulating motion of a spacecraft are compared. The former approach involves integrating a system of nonlinear differential equations, the latter is based on the assumption that the resultant moment is zero. Illustrative examples are given to show the efficiency of the methods, and some additional approaches to the problem are considered.

Related Organizations

Johnson Space Center
United States
National Aeronautics and Space Administration
United States

Keywords

checking function, zero resultant moment, Orbital mechanics, Computational methods for problems pertaining to mechanics of particles and systems, system of nonlinear differential equations

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Fields of Science (3) View all

engineering and technology

mechanical engineering

Fields of Science

engineering and technology

mechanical engineering

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