Based on minimal fuel principle, the switching curve of ignition is confirmed by using optimization theory, and a braking scheme is designed for the process of the lunar probe vertical soft landing.
针对月球探测器垂直软着陆过程，基于耗燃最优的原则，利用最优化理论确定了点火切换曲线。设计出一种制动方案。
Software design includes: writing programs of rotate speed computing module, ignition timing computing module and ignition control module and curve fitting.
软件设计部分包括转速计算模块、点火时间计算模块、点火控制模块和曲线拟合等的程序编写。
On the basis of ignition heating up curve, the ignition procedure is divided into three stages-heating, firing and burning.
根据点火曲线，可将其分为加热、着火和燃烧三个阶段。
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