Pages that link to "Item:Q597206"
From MaRDI portal
The following pages link to 3D geosynchronous transfer of a satellite: Continuation on the thrust (Q597206):
Displaying 13 items.
- Geometric optimal control and applications to aerospace (Q1704042) (← links)
- Optimal apogee burn time for low thrust spinning satellite in low altitude (Q1926949) (← links)
- Optimal control and applications to aerospace: some results and challenges (Q1937020) (← links)
- Optimal injection of a satellite into geostationary orbit using a limited number of thruster firings (Q2017634) (← links)
- Existence domain for solutions of optimal control problems for bounded-thrust spacecrafts (Q2314243) (← links)
- Minimum fuel control of the planar circular restricted three-body problem (Q2375759) (← links)
- Riemannian metric of the averaged energy minimization problem in orbital transfer with low thrust (Q2466256) (← links)
- Solution space exploration of low-thrust minimum-time trajectory optimization by combining two homotopies (Q2682341) (← links)
- Sensitivity analysis for time optimal orbit transfer (Q2747934) (← links)
- Differential continuation for regular optimal control problems (Q2885469) (← links)
- Homotopy method for minimum consumption orbit transfer problem (Q3416742) (← links)
- Second order optimality conditions in the smooth case and applications in optimal control (Q3593246) (← links)
- Remarks on Quadratic Hamiltonians in Spaceflight Mechanics (Q5436787) (← links)