大攻角条件下制导弹滚转稳定控制方法

Engineering

• Sliding Mode 100%
• Angle-of-Attack 100%
• External Disturbance 50%
• Feedback Control System 50%
• Finite Time 50%
• Simulated Result 50%
• Nonlinearity 50%
• Aerodynamic Model 50%
• Parameter Uncertainty 50%
• Convergence Property 50%