Solution of the problem of interplanetary-probe approach to several asteroids using an optimal-correction algorithm

Details Solution of the problem of interplanetary-probe approach to several asteroids using an optimal-correction algorithm Solution of the problem of interplanetary-probe approach to several asteroids using an optimal-correction algorithm

Jul 1988

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1988kosis..26..508z&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 26, July-Aug. 1988, p. 508-518. In Russian.

Physics

Asteroids, Earth-Mars Trajectories, Interplanetary Navigation, Orbital Elements, Transfer Orbits, Velocity Distribution

Scientific paper

An interactive procedure for solving an approach problem with N asteroids of the main belt is considered for an earth-Mars transfer trajectory with flyby of selected asteroids. The asteroid approach is realized using jet impulses with a total loss of characteristic velocity w. A solution is obtained to the problem of selecting the asteroids and the program of impulses minimizing w. A simplex algorithm of optimal linear impulse correction is used for the minimization of w.

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