Modal control of a satellite in an unstable orbit about L3

Details Modal control of a satellite in an unstable orbit about L3 Modal control of a satellite in an unstable orbit about L3

Dec 1982

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1982aifo.reptt....d&link_type=abstract

M.S. Thesis Air Force Inst. of Tech., Wright-Patterson AFB, OH. School of Engineering.

Physics

Equatorial Orbits, Many Body Problem, Perturbation Theory, Satellite Orientation, Perturbation, Polar Orbits, Trajectories

Scientific paper

A perturbation analysis was done on a satellite in orbit about Language point 3. A modal control scheme for linear systems was then applied to the linear and nonlinear perturbations. Rectification of the satellite orbit was achieved by Encke's Method. The effects of the Moon's inclination and eccentricity on the orbit stability was investigated. The controller stabilized the linear and nonlinear perturbations, with the average control acceleration being of the same order of magnitude as that for Earth-synchronous satellites.

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