基于hp伪谱同伦凸优化的火箭垂直回收在线轨迹规划方法

Engineering

• Optimisation Problem 100%
• Trajectory Planning 100%
• Estimation Time 100%
• Simulation Result 50%
• Optimization Method 50%
• Computational Efficiency 50%
• Fixed Points 50%
• Interior Point 50%
• Convergence Performance 50%
• Economic Efficiency 50%
• Linear Time 50%
• Reusable Launch Vehicle 50%
• Point Method 50%