基于偏置比例导引与凸优化的火箭垂直着陆制导

Engineering

• Launch Vehicles 100%
• Receding Horizon Control 100%
• Simulation Result 50%
• Engineering 50%
• Optimization Method 50%
• Nonlinearity 50%
• Convex Optimization Problem 50%
• Optimal Control Problem 50%
• Combined Method 50%
• Terminal Velocity 50%