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The two-body problem with drag and radiation pressure
Authors:A. G. Mavraganis  D. G. Michalakis
Affiliation:(1) Dept. of Engineering Science, Section of Mechanics, National Technical University of Athens, Greece
Abstract:The Kepler problem including radiation pressure and drag is treated. The equation of the orbit is derived and the scalar and vector integrals of motion are obtained by direct operation on the vector form of the equation of motion.
Keywords:Radiation pressure  atmospheric drag
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