Space debris delta-velocity probability density function was deduced by NASA's standard breakup model, and time integral algorithm of collision probability between spacecraft and any debris was built.
推导了基于NASA标准解体模型的碎片分离速度概率密度函数，建立了计算航天器与单颗碎片碰撞概率的时间积分算法。
Using integral algorithm to realize the computing of braking speed and braking distance and time.
利用积分算法，实现了对瞬时速度、制动距离和制动时间的测量。
Four acceleration techniques are employed to achieve integral algorithm optimisation for ensuring real-time simulation effects.
为了保证游戏实时性，采取四种加速策略进行整体算法优化。
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