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本帖最后由 一身轻松 于 2013-10-16 23:45 编辑
1 I: o3 i8 q% Q9 Q& [1 ~. j5 m* uxlan1976 发表于 2013-10-16 23:30 ; [5 U3 x9 J! y; a7 |, g, A
。。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 ... 4 V) E j3 v2 C
6 C+ W# r. p3 v3 q9 v7 L) OThe 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]. w: ^; F# I+ _6 e; D+ @
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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. R6 X Z" L% a7 N2 F) y% \
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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.
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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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