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本帖最后由 一身轻松 于 2013-10-16 23:45 编辑 + E5 L- X+ C/ c- H1 f# S
xlan1976 发表于 2013-10-16 23:30 $ y$ j1 L* |+ q! Y
。。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 ... 1 y3 ]' A6 Q3 p' Z4 n+ T/ d5 u2 v/ Y6 y
# @! r6 e, a/ ^2 o+ ZThe 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]. {3 h1 K3 X3 g" T$ \$ A4 U0 C9 R
9 ^& [) g, u( m3 O H) ?6 uThe 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.
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8 K3 `9 f; z% D8 m: [The 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.) l ^$ s+ ~, I0 P; P. M
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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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