Physics
Scientific paper
Jul 1982
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1982kosis..20..499i&link_type=abstract
Kosmicheskie Issledovaniia, vol. 20, July-Aug. 1982, p. 499-504, In Russian.
Physics
Optimal Control, Orbital Rendezvous, Spacecraft Control, Spacecraft Orbits, Trajectory Optimization, Circular Orbits, Spacecraft Motion
Scientific paper
The paper examines the coplanar rendezvous of a maneuvering spacecraft with a passive spacecraft in a circular orbit. It is assumed that a control acceleration of limited magnitude is imposed on the active spacecraft, and that its direction changes in accordance with a fuel-optimal control law. An analytical solution is sought for the corresponding variational problem in a finite form, with specified constraints on the rendezvous time. An optimal relationship is obtained for changes of the tangent of the angle of the control-acceleration vector in the form of a fractional-linear function of time.
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