航天系统. LV/SC分离后的相对运动分析要素

[中文适用范围]： 本国际标准提供了运载火箭/航天器分离后相对运动分析的要素，包括分析输入、原理、方法和输出。适用于运载火箭/航天器分离任务设计与验证中的相对运动预测。本国际标准侧重于单一发射任务中涉及对象之间的相对运动，并不涵盖新发射物体与在轨物体间的碰撞 avoidance 问题。 [外文原描述]： ISO 16679:2015 provides relative motion analysis elements after LV/SC separation, including analysis input, analysis principle, analysis method and analysis output. It is applicable to the mission design and verification for the prediction of relative motion after LV/SC separation. This International Standard focuses on the relative motion between the objects involved in one launch mission. It does not cover the issues about the collision avoidance between newly launched objects and on-orbit ones.