Physics
Scientific paper
Nov 1975
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975kosis..13..812g&link_type=abstract
Kosmicheskie Issledovaniia, vol. 13, Nov.-Dec. 1975, p. 812-816. In Russian.
Physics
Earth-Moon Trajectories, Moon-Earth Trajectories, Orbital Velocity, Trajectory Optimization, Transfer Orbits, Command And Control, Optimal Control, Satellite Control, Satellite Orbits
Scientific paper
Transfer trajectories from artificial earth satellite orbits to artificial moon satellite orbits and vice versa, with minimum characteristic velocities, are discussed with the constraints of fixed transfer time, free orientation of the orbit planes for either type of satellite orbit, and a variation in power-on acceleration in the gravitational field of a nonspherical earth, the moon, and the sun. Minimum expenditures of the characteristic velocity in the orbit transfer are required. Deviations of the trajectory based on a prior command program from the absolute optimum trajectory are considered. Two-impulse transfers are found optimal.
Gurman V. I.
Gusev L. I.
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