【摘要】 火箭弹、旋转导弹和炮弹起始扰动的形式不能直接引入旋转飞行器刚体弹道模型中,需对其进行变换,分析了风对旋转飞行器运动的影响,得到了有风存在时起始攻角和起始侧滑角的公式,并且得到了刚体弹道模型中三个起始轴向扰动角速度的公式。更多还原

【Abstract】 Disturbances of rockets,rolling missiles and projectiles can’t be introduced into rigid body trajectory models of rolling flying vehicles without transformation.The influence of wind on the rolling flying vehicle motion is analyzed.The formulae of initial angle of attack and angle of sideslip,and the formulae of the three initial angular rate disturbance in rigid body trajectory models are obtained.更多还原