本文介绍了用于进气道风洞试验的微型计算机控制系统。其特点是:整个控制过程程序化,能实现显示控制对象的位置,可据两维空间状态控制的不同要求,只要在程序上稍加修改便可适用。经一期进气道试验表明:性能可靠,精度高,灵活性大。 This article describes a microcomputer control system for inlet wind tunnel testing. Its characteristics are: the entire process of control procedures, to achieve the position of the display control object, according to the two-dimensional space state control of different requirements, as long as the program can be amended slightly applicable. After a period of inlet test shows: reliable performance, high precision and flexibility.