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- W4384834251 abstract "The paper considers the optimization of interplanetary flight to Mars in the impulse statement. The flight schemes with and without perturbation maneuver near the Moon are compared. The trajectories are considered as sets of Lambert's problems and are optimized by gradient methods. Taking into account only one attracting center at each section of the trajectory, the scheme with a maneuver near the Moon allows gaining about 150 m/s in characteristic velocity." @default.
- W4384834251 created "2023-07-21" @default.
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- W4384834251 date "2023-05-29" @default.
- W4384834251 modified "2023-09-23" @default.
- W4384834251 title "On Constructing the Trajectory of Spacecraft Flight to Phobos with a Perturbation Maneuver near the Moon, Based on the Solution of a Combination of 4 Lambert’s Problems" @default.
- W4384834251 cites W1967161631 @default.
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- W4384834251 doi "https://doi.org/10.23919/icins51816.2023.10168493" @default.
- W4384834251 hasPublicationYear "2023" @default.
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