Comprehensive Six-Degrees-of-Freedom Trajectory Design and Optimization of a Launch Vehicle with a Hybrid Last Stage Using the PSO Algorithm

Keyphrases

• Six Degrees of Freedom 100%
• PSO Algorithm 100%
• Trajectory Design 100%
• Trajectory Optimization 100%
• Launch Vehicle 100%
• Propulsion Performance 16%
• Cost Reduction 16%
• Overall Cost 16%
• Detailed Design 16%
• Particle Swarm Optimization 16%
• Center of Gravity 16%
• Moment of Inertia 16%
• Vehicle Geometry 16%
• Weight Ratio 16%
• Vehicle Performance 16%
• Increased Performance 16%
• Innovative Study 16%
• Percentage Difference 16%
• Aerodynamic Coefficients 16%
• Hybrid Rocket Motor 16%
• Flight Path Angle 16%
• Specific Impulse 16%
• Handling Cost 16%
• Vehicle Trajectory 16%
• Launch System 16%
• Minotaur 16%
• Precision Design 16%
• Hybrid Motor 16%
• Motor Selection 16%
• Total Impulse 16%
• Design Problems 16%

Engineering

• Degree of Freedom 100%
• Launch Vehicle 100%
• Particle Swarm Optimization 16%
• Rocket Engine 16%
• Aerodynamic Coefficient 16%
• Flight Path Angle 16%
• Specific Impulse 16%
• Design Problem 16%
• Hybrid Motor 16%
• Moment of Inertia 16%