Geometrical solution of a rendezvous problem on close, almost-circular, coplanar orbits

Details Geometrical solution of a rendezvous problem on close, almost-circular, coplanar orbits Geometrical solution of a rendezvous problem on close, almost-circular, coplanar orbits

Nov 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989kosis..27..808b&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 27, Nov.-Dec. 1989, p. 808-816. In Russian.

Astronomy and Astrophysics

Astronomy

1

Astrodynamics, Circular Orbits, Coplanarity, Orbital Rendezvous, Algorithms, Impulses, Iteration, Linear Equations, Roots Of Equations

Scientific paper

Two-, three-, and four-impulse maneuvers assuring the soft rendezvous of two space vehicles are examined in the linear formulation. The impulses are applied at two maneuever segments, the distance between which amounts to several loops. Algorithms are proposed which can be used to determine the application angles and components of impulses in the case of which the total characteristic velocity of the maneuver is minimal.

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