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引 言 1964年,在“阿波罗”计划中采纳了重要的决定:全部控制工序的实行要借助于飞船上的数字计算机。应指出,在以前所有的载人宇宙飞行中是使用模拟控制系统。本文将论述登月舱控制系统的设计。控制系统最复杂的部分是数字稳定系统,因此,为了设计此系统需要发展新的方法。 本文的目的是研究在设计过程中出现的一些问题。在许多情况下,由于系统成本和研制时间的限制,使实际的控制系统与理论出现了差异。
Introduction In 1964, an important decision was taken in the “Apollo” project: the entire control process was implemented with the aid of a digital computer onboard the spacecraft. It should be noted that in all previous manned space missions simulation control systems were used. This article will discuss the design of the lunar module control system. The most complex part of the control system is the digital stabilization system, so new ways need to be developed to design this system. The purpose of this article is to study some issues that arise during the design process. In many cases, the actual control system differs from the theory due to the limitation of system cost and development time.