Rendezvous of low-thrust spacecraft in a near-circular orbit

Details Rendezvous of low-thrust spacecraft in a near-circular orbit Rendezvous of low-thrust spacecraft in a near-circular orbit

Mar 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992kosis..30..165i&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 30, no. 2, Mar.-Apr. 1992, p. 165-179. In Russian.

Computer Science

Circular Orbits, Equations Of Motion, Low Thrust, Spacecraft Motion, Thrust Vector Control, Optimal Control, Rendezvous Trajectories, Spacecraft Control, State Vectors

Scientific paper

The problem of the rendezvous of low-thrust spacecraft in near-circular orbits is considered. A simplified model of motion is derived on the basis of motion equations linearized by the selection of slowly changing and periodic components. The general problem is divided into individual ones, namely, control of transversal and longitudinal motion and control of slowly changing and periodic components. A number of local optimal control programs for the transversal and free orientation of the thrust vector are obtained as a speed-of-response criterion. The efficiency of the control programs obtained is evaluated.

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