The rotation of a rigid body satellite near the Lagrangian point L4

Details The rotation of a rigid body satellite near the Lagrangian point L4 The rotation of a rigid body satellite near the Lagrangian point L4

Aug 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986asdy.conf..781e&link_type=abstract

IN: Astrodynamics 1985; Proceedings of the Conference, Vail, CO, August 12-15, 1985. Part 2 (A86-43201 20-12). San Diego, CA, Un

Astronomy and Astrophysics

Astronomy

Lagrangian Equilibrium Points, Satellite Perturbation, Satellite Rotation, Three Body Problem, Hill Method, Librational Motion, Rigid Structures

Scientific paper

This paper deals with the problem of rotation of a rigid body about the center of mass, near the triangular libration point L4 of the restricted circular three-body problem. It is assumed that the orbit of the center of mass of the satellite is a known function of the time. The first-order perturbation method is employed, with angle-action variables for the rotational motion of a triaxial satellite.

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