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In low Earth orbit, say 220 miles (355 km) up, where most human space travel takes place, a single circuit is completed in a much brisker 90 minutes.
在近地轨道,例如高于地球表面220英里(355公里)处大多数人类太空旅行发生的地方,运行一圈则需要更短的90分钟。
The present paper discussed the overall design scheme of this system, including the designs of generating sector, receiver sector, single circuit initiating.
本文论述了系统设计的总体方案,发射端、接收端和单路起爆电路的设计,以及系统实现的方法和原理。
By using the waning curve method, an adjustment method of the single circuit control system adjuster parameters is obtained.
利用衰减曲线法,得出单回路控制系统调节器参数的整定方法。
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