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本文导出探空火箭速度方向角(俯仰角)和方位角(偏航角)满足的一组微分方程,并在一些近似假定下分析了风对探空火箭飞行弹道的影响。
In this paper, we derive a set of differential equations satisfied by the velocity and azimuth angles of the sounding rocket, and analyze the effect of the wind on the flight trajectory of the sounding rocket under some approximate assumptions.