Based on the great orbit-transfering velocity increment and less intercepting time of kinetic weapon in space, this dissertation brings a new method of determining a predictive interception point.
针对天基动能武器速度增量大、拦截时间小的特性,提出了一种新的确定预测拦截点的方法。
Based on the great orbit-transfering velocity increment and less intercepting time of kinetic weapon in space, this dissertation brings a new method of determining a predictive interception point.
针对天基动能武器速度增量大、拦截时间小的特性,提出了一种新的确定预测拦截点的方法。
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