基于多模型网络的激光末制导炮弹诸元解算方法

Engineering

• Network Model 100%
• Terminal Guidance 100%
• Air Temperature 66%
• Air Pressure 66%
• Simulation Result 33%
• Obtains 33%
• Degree of Freedom 33%
• Defects 33%
• Least Square 33%
• Deep Neural Network 33%
• Error Rate 33%
• Square Method 33%
• Initial Condition 33%
• Flight Test 33%
• Truncation Error 33%
• Accurate Solution 33%