Computer Science
Scientific paper
Dec 1981
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981aifo.rept.....e&link_type=abstract
M.S. Thesis Air Force Inst. of Tech., Wright-Patterson AFB, OH. School of Engineering.
Computer Science
Lunar Gravitational Effects, Satellite Orbits, Satellite Perturbation, Computerized Simulation, Equations Of Motion, Fourier Analysis, Vector Analysis
Scientific paper
A Fourier representation of the perturbation effects of the Moon's eccentricity on a satellite in orbit about L3 was constructed and verified numerically. It was then incorporated in a modal control scheme for linear systems that are time periodic which was developed by Shelton. The feasibility of this modified control scheme was then verified by computer simulation by controlling the actual nonlinear motions of the satellite with the modified controller.
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