Optimal motion of spacecraft in vicinity of Kepler ellipse of arbitrary eccentricity

Details Optimal motion of spacecraft in vicinity of Kepler ellipse of arbitrary eccentricity Optimal motion of spacecraft in vicinity of Kepler ellipse of arbitrary eccentricity

Nov 1974

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1974kosis..12..353l&link_type=abstract

(Kosmicheskie Issledovaniia, vol. 12, May-June 1974, p. 353-359.) Cosmic Research, vol. 12, no. 3, Nov. 1974, p. 324-330. Trans

Physics

Eccentric Orbits, Elliptical Orbits, Gravitational Effects, Kepler Laws, Spacecraft Motion, Trajectory Optimization, Differential Equations, Equations Of Motion, Extremum Values, Fuel Consumption, Optimal Control, Orbit Perturbation, Planetary Gravitation, Vertical Motion

Scientific paper

(Previously cited in issue 16, p. 2344, Accession no. A74-35073)

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