Pages that link to "Item:Q933832"
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The following pages link to Optimal starting conditions for the rendezvous maneuver. II: Mathematical programming approach (Q933832):
Displaying 3 items.
- Necessary and sufficient conditions of the rendezvous between a single spacecraft and three non-coplanar Walker constellation satellites (Q413132) (← links)
- Optimal starting conditions for the rendezvous maneuver. I: Optimal control approach (Q933828) (← links)
- Rendezvous phasing special-point maneuvers mixed discrete-continuous optimization using simulated annealing (Q4929529) (← links)