Optimization of Flight Trajectories of a Spacecraft with Electric Propulsion Using the Gravitational Maneuver

Details Optimization of Flight Trajectories of a Spacecraft with Electric Propulsion Using the Gravitational Maneuver Optimization of Flight Trajectories of a Spacecraft with Electric Propulsion Using the Gravitational Maneuver

Jul 2004

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2004cosre..42..389f&link_type=abstract

Cosmic Research, v. 42, Issue 4, p. 389-398 (2004).

Mathematics

Scientific paper

Necessary conditions of optimality of the use of a gravitational maneuver during a flight are obtained, and a mathematical model for its study is proposed. With the help of the developed method of optimization of a trajectory of an interplanetary flight using a favorable gravitational maneuver, estimations of a spacecraft's transport capabilities are made for flights to Mercury and for the delivery of a solar probe into the near vicinity of the Sun.

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