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本帖最后由 一身轻松 于 2013-10-16 23:45 编辑 & K A8 t d3 e9 f! N& ]
xlan1976 发表于 2013-10-16 23:30
5 e* @* m0 H% H9 M。。好吧。。我实在不知说什么了。。有F14的手册吗,拿出来晒晒,不然你这种明显违反常规的说法怎么能让 ... - q/ _- i6 n2 [& _7 ~
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The Central Air Data Computer is the integrated flight control system used in the early versions of the US Navy's F-14 Tomcat fighter. It is notable for its early use of a custom-designed MOS-based LSI microprocessor chipset, the MP944.[1]* ?% o* \7 L1 a0 {
. l, c S& d2 e3 F' M. @2 W% oThe CADC was designed and built at Garrett AiResearch by a team led by Steve Geller and Ray Holt, and supported by the startup American Microsystems. Design work started in 1968 and was completed in June 1970, beating out a number of electromechanical systems that had also been designed for the F-14.: L) @+ m X" ]4 [& ?& T
# j) ?4 r. {8 b9 nThe CADC consisted of an A-to-D converter, several quartz pressure sensors, and the MOS-based microprocessor. Inputs to the system included the primary flight controls, a number of switches, static and dynamic air pressure (for calculating stall points and aircraft speed) and a temperature gauge. The outputs controlled the primary flight controls, wing sweep, the F-14's leading edge "glove", and the flaps.
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7 Y4 D$ Y$ ^4 L7 B你说不是软件问题,可事实就是软件问题,因为F-14的机翼变角明显不是手动控制的。而且F-14的大气计算机很明显一种整合过了的飞行控制系统 |
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