Low-Thrust Trajectory Design with Successive Convex Optimization for Libration Point Orbits

Physics

• Optimization 100%
• Three Body Problem 50%
• Transferring 33%
• Halos 33%
• Non-Linear Dynamics 33%
• Space Missions 33%
• Lagrangian Points 33%
• Low Thrust Propulsion 33%
• Model 16%
• Stability 16%
• Independent Variables 16%
• Utilization 16%
• Correction 16%
• Fuel 16%
• Maneuvers 16%
• Ephemeris 16%

Engineering

• Lagrange Point 16%