Pages that link to "Item:Q5962793"
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The following pages link to Combined low-thrust propulsion and invariant manifold trajectories to capture NEOs in the Sun-Earth circular restricted three-body problem (Q5962793):
Displaying 5 items.
- Alternative transfers to the NEOs 99942 apophis, 1994 WR12, and 2007 UW1 via derived trajectories from periodic orbits of family G (Q966249) (← links)
- Direct and indirect capture of near-Earth asteroids in the Earth-Moon system (Q1682183) (← links)
- Long-term capture orbits for low-energy space missions (Q1785913) (← links)
- Using invariant manifolds to capture an asteroid near the \(L_3\) point of the Earth-Moon bicircular model (Q2045999) (← links)
- Transit and capture in the planar three-body problem leveraging low-thrust invariant manifolds (Q2049204) (← links)
