弹性细长旋转弹箭不同转速下的滚转共振特性研究
Journal of Projectiles,Rockets,Missiles and Guidance(2006)
Abstract
以推导出的考虑弹性影响条件下的尾翼式旋转导弹运动方程为基础,应用MATLAB编制程序,用有限元法对方程进行数值求解。对简化后的导弹模型的滚转共振现象和旋转自锁点的稳定性进行了分析,并应用上述方法分析某高速导弹的飞行特性。
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Key words
resonance,finite element method,lockin
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