Pages that link to "Item:Q1578840"
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The following pages link to Very low-thrust trajectory optimization using a direct SQP method (Q1578840):
Displaying 18 items.
- Low-thrust trajectory optimization in a full ephemeris model (Q318431) (← links)
- Mathematical modeling of spacecraft guidance and control system in 3D space orbit transfer mission (Q338285) (← links)
- Multi-swingby optimization of mission to Saturn using global optimization algorithms (Q358717) (← links)
- Orbital transfers: optimization methods and recent results (Q428488) (← links)
- Review of formulations for structural and mechanical system optimization (Q438513) (← links)
- Trajectory optimization for maneuvering satellites (Q759998) (← links)
- Optimal multi-objective low-thrust spacecraft trajectories (Q1574399) (← links)
- Halo orbit mission correction maneuvers using optimal control (Q1613163) (← links)
- A full-space quasi-Lagrange-Newton-Krylov algorithm for trajectory optimization problems (Q1638023) (← links)
- Optimal space trajectories with multiple coast arcs using modified equinoctial elements (Q2055347) (← links)
- Meyer wavelet neural networks to solve a novel design of fractional order pantograph Lane-Emden differential model (Q2169713) (← links)
- Multi-objective low-thrust spacecraft trajectory design using reachability analysis (Q2681188) (← links)
- Low-Thrust Multi-Revolution Orbit Transfers (Q3133920) (← links)
- Flatness-Based Low-Thrust Trajectory Optimization for Spacecraft Proximity Operations (Q3133928) (← links)
- Several simultaneous formulations for transient dynamic response optimization: An evaluation (Q3649901) (← links)
- The solution of some difficult problems in low-thrust interplanetary trajectory optimization (Q3815978) (← links)
- (Q3833694) (← links)
- Optimal low‒thrust orbit transfers with eclipsing (Q5247900) (← links)
