给出再入飞行的假设条件，建立飞行器再入质心动力学及运动学模型。
Several assumptions to entry flight were listed, and entry dynamics were established.
在分析了本方案优点的基础上，建立了质量矩控制导弹的动力学模型，包括质心动力学和绕质心的动力学方程。
On basis of analyzing the advantages of the scheme, a dynamics model of MMTC was constructed, which includes centroid dynamics and dynamics moment equations of centroid.
应用推荐