类似的工作仿真了在进入轨道期间管理火箭引擎点火的运载火箭数字计算机(Launch Vehicle Digital Computer, LVDC)。
A similar effort simulates the launch vehicle digital computer (LVDC) that managed the firing of the rocket engines during ascent into orbit.
该点火系统实现数字式离心点火提前，结构简单，可以满足各种发动机对点火系统的要求。
The ignition system is digital controlled in centrifugal spark advance, simple in construction and is able to satisfy the demand of all kinds of engine 's ignition system.
数字点火方式具有适时性好、响应快、控制点火时刻更为精确等其他点火方式无法比拟的优点。
Compared with other ignition methods, digital ignition has the advantages of good adaptability, fast responsibility, and precise control of the time of ignition.
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