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本帖最后由 一身轻松 于 2013-10-16 23:45 编辑
1 Z. u3 d. F4 G" B, o: C6 o9 g1 gxlan1976 发表于 2013-10-16 23:30 ?) O, m% A7 I9 K0 w* [ 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 ... : B3 r- @8 R1 g/ \' \/ M$ F$ E
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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]
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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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3 A- b; O3 U* g3 q# [$ LThe 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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# y# [5 ^8 Y T6 `/ y: j9 F+ C5 D& ?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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