Qualitative Properties of Orbits for Minimum-Fuel Impulsive Transfers between Circular Coplanar Orbits with a Given Launch Time

Details Qualitative Properties of Orbits for Minimum-Fuel Impulsive Transfers between Circular Coplanar Orbits with a Given Launch Time Qualitative Properties of Orbits for Minimum-Fuel Impulsive Transfers between Circular Coplanar Orbits with a Given Launch Time

Publishing date

Sep 2003

URL

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2003cosre..41..443k&link_type=abstract

Journals

Cosmic Research, v. 41, Issue 5, p. 443-452 (2003).

Science

Physics

Type

Scientific paper

Abstract

The coplanar problem of minimizing propellant consumption in impulsive transfer between circular boundary orbits is investigated. The launch time and the initial configuration of objects on the boundary orbits are specified arbitrarily. The qualitative properties of optimal two-impulse trajectories and their optimality in the class of multi-impulse transfers are studied.

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