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本帖最后由 一身轻松 于 2013-10-16 23:45 编辑
E% S7 o1 d: @; b6 _+ G. ?xlan1976 发表于 2013-10-16 23:30
X, z! s' _$ {, J v7 ^3 o* ~/ X。。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/ M& K# A: V, x$ h$ q
- J: t m) }/ R6 ]3 F! [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]
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The 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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0 }! l. \+ a8 r3 n; L) C3 KThe 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.* b$ N8 P& E% Y [6 m1 e
0 e) A- X3 k* p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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