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用另一个卫星拦截轨道目标,是指两个飞行器必须同时到达空间的同一点。下述计算方法就是解决这个碰撞问题的。为了容易计算拦截轨道未知的长半轴,把朗贝尔方程改写成幂级数形式,就可用方便的微分校正技术来代替通常的试凑法进行计算。
Intercepting an orbital target with another satellite means that both aircraft must arrive at the same point in space at the same time. The following calculation is to solve this collision problem. In order to easily calculate the unknown long axis of the intercept track, the Lambert equation can be rewritten as a power series instead of the usual trial and error method using a convenient differential correction technique.