Online Reentry Trajectory Optimization Using Modified Sequential Convex Programming for Hypersonic Vehicle

Engineering

• Computer Simulation 50%
• Continuous Time 50%
• Demonstrates 50%
• Dynamic Pressure 50%
• Heat Rate 50%
• Hypersonic Vehicles 100%
• Objective Function 100%
• Optimal Control 50%
• Optimality 100%
• Optimisation Problem 50%
• Pressure Load 50%
• State Equation 50%
• Taylor Series Expansion 50%

Mathematics

• Continuous Time 25%
• Convex Programming 100%
• Convex Programming Problem 25%
• Numerical Simulation 25%
• Objective Function 50%
• Optimal Control Theory 25%
• Optimality 50%
• State Equation 25%
• Taylor Series Expansion 25%

Computer Science

• continuous-time 20%
• Convex Programming 100%
• Dynamic Pressure 20%
• Fast Convergence 20%
• Numerical Simulation 20%
• Objective Function 40%
• Optimization Problem 20%
• Path Constraint 20%
• Programming Method 20%
• State Equation 20%
• Taylor Series Expansion 20%