Perturbations of the motion of the center of mass of a spacecraft given by the motion around the center of mass

Details Perturbations of the motion of the center of mass of a spacecraft given by the motion around the center of mass Perturbations of the motion of the center of mass of a spacecraft given by the motion around the center of mass

Dec 1985

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1985stcma..44..555s&link_type=abstract

Studii si Cercetari de Mecanica Aplicata (ISSN 0039-4017), vol. 44, Nov.-Dec. 1985, p. 555-568. In Romanian.

Astronomy and Astrophysics

Astronomy

Astrodynamics, Center Of Mass, Gravitational Effects, Orbit Perturbation, Spacecraft Orbits, Orbital Elements, Rigid Structures

Scientific paper

The motion of the center of mass of a spacecraft, considered a rigid body, under the effect of a gravitational center is analyzed. Newton's equations are used for the variation of the orbital elements, showing the trajectory perturbations of the center of mass. Two particular cases are studied: (1) the rapid rotation, and (2) the gravitational stabilization.

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