The problem of approaching several asteroids

Details The problem of approaching several asteroids The problem of approaching several asteroids

Jan 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989kosis..27....3z&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 27, Jan.-Feb. 1989, p. 3-8. In Russian.

Physics

Asteroids, Interplanetary Flight, Moon-Earth Trajectories, Spacecraft Trajectories, Trajectory Optimization, Algorithms, Error Correcting Devices, Iteration, Mars (Planet), Swingby Technique

Scientific paper

The work of Zhirnov and Lidov (1983) on the problem of a single space probe approaching several asteroids is extended. Examples of the approach of N asteriods with N = 2,3,4,5 is considered. Variants are indicated in which the characteristic approach velocity w sub N for N asteriods does not exceed w sub 2 = 0.069, w sub 3 = 0.255, w sub 4 = 0.611, and w sub 5 = 1.36 km/s. A numerical iterative procedure for solving the nonlinear approach problem is implemented using a linear optimal correction algorithm.

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