Pages that link to "Item:Q3459280"
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The following pages link to Adjoints estimation methods for impulsive Moon-to-Earth trajectories in the restricted three-body problem (Q3459280):
Displaying 3 items.
- Optimal round trip lunar missions based on the patched-conic approximation (Q338274) (← links)
- Optimal two-impulse trajectories with moderate flight time for Earth-Moon missions (Q1955429) (← links)
- A study of Earth-Moon trajectories based on analytical expressions for the velocity increments (Q2313872) (← links)