Optimization of Flight Trajectories of a Spacecraft with Electric Propulsion Using the Gravitational Maneuver |
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Authors: | Fedotov G. G. |
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Affiliation: | (1) Moscow State Aviation Institute (University of Aerospace Technology), Volokolamskoe sh. 4, Moscow, 125993, Russia |
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Abstract: | 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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