Pages that link to "Item:Q933828"
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The following pages link to Optimal starting conditions for the rendezvous maneuver. I: Optimal control approach (Q933828):
Displaying 10 items.
- Necessary and sufficient conditions of the rendezvous between a single spacecraft and three non-coplanar Walker constellation satellites (Q413132) (← links)
- Optimal switching strategy for radially accelerated trajectories (Q642325) (← links)
- Multiple spacecraft rendezvous maneuvers by differential drag and low thrust engines (Q642338) (← links)
- Optimal starting conditions for the rendezvous maneuver. II: Mathematical programming approach (Q933832) (← links)
- Optimal trajectories for spacecraft rendezvous (Q946319) (← links)
- Guidance trajectories for spacecraft rendezvous (Q946320) (← links)
- A new approach to impulsive rendezvous near circular orbit (Q1955964) (← links)
- Optimization of the proportional navigation law with time delay (Q2378115) (← links)
- On Verification of fuel-optimal space trajectories (Q3809681) (← links)
- Rendezvous phasing special-point maneuvers mixed discrete-continuous optimization using simulated annealing (Q4929529) (← links)