Pages that link to "Item:Q622326"
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The following pages link to Geometric and numerical techniques in optimal control of two and three-body problems (Q622326):
Displaying 11 items.
- Optimization of the forcing term for the solution of two-point boundary value problems (Q355817) (← links)
- Designing rendezvous missions with mini-moons using geometric optimal control (Q380585) (← links)
- Metrics with equatorial singularities on the sphere (Q466949) (← links)
- Shooting and numerical continuation methods for computing time-minimal and energy-minimal trajectories in the Earth-Moon system using low propulsion (Q765005) (← links)
- Geometric optimal control of elliptic Keplerian orbits (Q812846) (← links)
- Time versus energy in the averaged optimal coplanar Kepler transfer towards circular orbits (Q2340512) (← links)
- Bifurcations of the conjugate locus (Q2360610) (← links)
- Energy minimization of single input orbit transfer by averaging and continuation (Q2370811) (← links)
- Minimum fuel control of the planar circular restricted three-body problem (Q2375759) (← links)
- Averaging and optimal control of elliptic keplerian orbits with low propulsion (Q2433415) (← links)
- Continuation from a flat to a round Earth model in the coplanar orbit transfer problem (Q2864787) (← links)
