载机滚转条件下的导弹弹射分离横向位移研究

Engineering

• Engineering 100%
• Lateral Displacement 100%
• Active Control 50%
• Air-to-Air Missile 50%
• Dynamic Model 50%
• Actuation 50%
• Lagrange Equation 50%
• Coriolis Effect 50%
• Lateral Deformation 50%