基于高斯伪谱法的二级助推战术火箭多阶段轨迹优化

Engineering

• Multistage 100%
• Gauss 100%
• Boosters (Rocket) 100%
• Initial Value 66%
• Demonstrates 33%
• Optimization Method 33%
• Simulated Result 33%
• Numerical Example 33%
• Optimisation Problem 33%
• Computational Efficiency 33%
• Contact Point 33%
• Optimal Trajectory 33%
• Multiple Constraint 33%
• Flight Phase 33%
• Operating Characteristic 33%