Concerning a property of three-impulse trajectories, optimal with constraints on transfer distance and time

Details Concerning a property of three-impulse trajectories, optimal with constraints on transfer distance and time Concerning a property of three-impulse trajectories, optimal with constraints on transfer distance and time

May 1982

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1982kosis..20..352i&link_type=abstract

Kosmicheskie Issledovaniia, vol. 20, May-June 1982, p. 352-256. In Russian.

Physics

Spacecraft Maneuvers, Trajectory Optimization, Transfer Orbits, Circular Orbits, Constraints, Fuel Consumption, Gravitational Fields

Scientific paper

The paper examines fuel-optimal multiimpulse transfers of a spacecraft between coplanar circular orbits in a central Newtonian gravitational field. There are constraints on the distance of the spacecraft from the center of attraction and on the transfer time. The initial and final orbits are such that, given free transfer-time and a constraint on the distance, the optimal transfer will be a three-impulse one with an intermediate impulse at the outer boundary. In the case of constrained transfer time, the intermediate impulse is applied when the spacecraft is at its present distance from the center of attraction.

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