The mechanism of spin motion and the function of various control surfaces are explored during the aircraft entry into and recovery from, a spin.
探讨其运动机理以及各操纵面在尾旋进入和改出中的作用。
Finally, we compare six degrees of freedom simulation results of ballistic re-entry missiles motion with the computing results of approximate formula. The comparison shows the feasibility...
最后用六自由度弹道数字仿真结果同近似计算结果作了比较,比较结果表明了近似分析的可行性。
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