标准编号：ISO 16679:2015
中文名称：航天系统 运载火箭/宇宙飞船分离后相对运动分析要素
英文名称：Space systems — Relative motion analysis elements after LV/SC separation
发布日期：2015-09
标准范围
This International Standard provides relative motion analysis elements after LV/SC separation,including analysis input, analysis principle, analysis method and analysis output. It is applicable to themission 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 launchmission. It does not cover the issues about the collision avoidance between newly launched objects andon-orbit ones.
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