Pages that link to "Item:Q1955429"
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The following pages link to Optimal two-impulse trajectories with moderate flight time for Earth-Moon missions (Q1955429):
Displaying 13 items.
- Optimal round trip lunar missions based on the patched-conic approximation (Q338274) (← links)
- Searching for orbits with minimum fuel consumption for station-keeping maneuvers: an application to lunisolar perturbations (Q473630) (← links)
- Station keeping of constellations using multiobjective strategies (Q473700) (← links)
- Characteristic analysis and design of near Moon abort trajectory for manned lunar landing mission (Q546388) (← links)
- Using a three-impulse maneuvering scheme for returning from the lunar orbit to the reentry point of the Earth's atmosphere (Q786152) (← links)
- Optimal trajectories for Earth-to-Mars flight (Q1379928) (← links)
- Minimum fuel trajectories for round trip lunar missions (Q1993639) (← links)
- A study of Earth-Moon trajectories based on analytical expressions for the velocity increments (Q2313872) (← links)
- Application of a genetic algorithm in orbital maneuvers (Q2516814) (← links)
- Pareto frontier for the time-energy cost vector to an Earth-Moon transfer orbit using the patched-conic approximation (Q2516818) (← links)
- Adjoints estimation methods for impulsive Moon-to-Earth trajectories in the restricted three-body problem (Q3459280) (← links)
- (Q4665085) (← links)
- Energy analysis of the single impulsive Earth-Moon transfer with the temporary lunar capture (Q6177817) (← links)
