An algorithm for calculating the parameters of multiple-circuit distant-aim maneuvers

Details An algorithm for calculating the parameters of multiple-circuit distant-aim maneuvers An algorithm for calculating the parameters of multiple-circuit distant-aim maneuvers

Jan 1990

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1990kosis..28...69b&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 28, Jan.-Feb. 1990, p. 69-76. In Russian.

Computer Science

Numerical Analysis

Active Satellites, Algorithms, Orbital Rendezvous, Spacecraft Maneuvers, Trajectory Optimization, Circular Orbits, Gravitational Effects, Numerical Analysis, Thrust Programming

Scientific paper

An analysis is made of four-impulse distant-aim maneuvers assuring a soft rendezvous of the active spacecraft with the target, which are moving in close nearly circular orbits. A numerical-analytical approach is used to construct an algorithm for determining the parameters of optimal maneuvers in a class of solutions for which the signs of all the transversal impulses coincide. A geometrical interpretation of the process of searching for the solution is given.

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