The invention relates to a carrier and carried vehicle separation attitude angle optimization method and device, and the method comprises the steps: calculating the motion state of each carried vehicle after separation according to the initial condition of a carrier injection moment; calculating the minimum value of the minimum distance between any two launched vehicles in the interval from the far-field analysis starting point moment to the terminal point moment based on the motion state of each launched vehicle after separation; calculating an included angle between a relative position vector of an upper stage of the carrier and a relay satellite and a normal of a phased-array antenna of the carrier according to the motion state of the carrier, and determining the total detectability of a separation attitude angle of the carrier by combining the condition that the upper stage of the carrier and the relay satellite are shielded by the earth; and optimizing the separation attitude angle based on the minimum value of the minimum distance between any two carried vehicles and the total detectability of the carrier separation attitude angle. The safety boundary requirement of the carried device is met, and the separation safety is ensured.
本申请涉及一种运载体与被运载器分离姿态角优化方法及装置,其包括,根据运载体入轨时刻的初始条件计算各被运载器分离后的运动状态;基于各被运载器分离后的运动状态计算远场分析起点时刻至终点时刻区间内任意两个被运载器之间最小距离的最小值;根据运载体运动状态计算运载体上面级与中继卫星的相对位置矢量与运载体相控阵天线法线之间的夹角并结合运载体上面级与中继卫星之间被地球遮挡的情况确定运载体分离姿态角的总可探测性;基于任意两个被运载器之间最小距离的最小值与运载体分离姿态角的总可探测性对所述分离姿态角进行优化。满足被运载器安全的边界要求,确保分离安全性。
Method and device for optimizing separation attitude angle of carrier and carried device
一种运载体与被运载器分离姿态角优化方法及装置
2022-12-20
Patent
Elektronische Ressource
Chinesisch
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