The application of the recurrent method of the extremum parabolic approximation to the problem of the optimum spacecraft behaviour.

Details The application of the recurrent method of the extremum parabolic approximation to the problem of the optimum spacecraft behaviour. The application of the recurrent method of the extremum parabolic approximation to the problem of the optimum spacecraft behaviour.

Aug 1990

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1990kosis..28..513v&link_type=abstract

Kosmicheskie Issledovaniia, Tom 28, Vyp. 4, p. 513 - 520

Physics

Space Vehicles: Encounters

Scientific paper

A recurrent method of approximation of the extremals for the determination of dynamic system behaviour during its fast transition from prescribed initial state to prescribed final state allowing for the limits of system movement characteristics is suggested. The problem of the spacecraft-satellite rendezvous is solved by means of the one-dimensional Pontryagin regulator for a two-dimensional system.

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