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本帖最后由 一身轻松 于 2013-10-16 23:45 编辑 ' r- D4 O* \6 i A' G
xlan1976 发表于 2013-10-16 23:30 ![]()
' M1 _0 m5 s x3 V' ^: L. 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 ... 2 \, j- m' b- o- T8 t
1 K7 ]0 u2 }7 Q$ N0 WThe 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]7 ?. K( \8 l: x, I
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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." V7 ~8 M7 N8 x2 D: b
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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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