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本文提出用雷达等设备测量飞行器在无动力段轨道上的位置矢量,把它和标称的轨道位置矢量加以比较,并对其差值用矩阵理论进行变换处理,可以确定飞行器上的制导系仪器在动力终止时刻的总制导误差。为精度鉴定提供了一种辅助方法,弥补了有动力段外弹道测量设备的某些不足,并可提供准确的重返大气层的标称轨道位置矢量,以鉴别再入误差。
This paper proposes to use the radar and other equipment to measure the position vector of the aircraft in orbit without power segment, compare it with the nominal orbit position vector, and transform the difference using the matrix theory to determine the position of the guidance system instrument Total guidance error at the end of power. This provides an additional method of accuracy identification that compensates for some of the deficiencies of powered off-range ballistic measuring equipment and provides an accurate nominal orbital position vector for return to the atmosphere to identify reentry errors.