|
本帖最后由 一身轻松 于 2013-10-16 23:45 编辑
9 N h# C& g! q8 S# ]3 ixlan1976 发表于 2013-10-16 23:30
" A/ [& j, A7 T# U) s o8 }+ i# x7 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 ...
, O7 I8 a9 p, [! D0 f
% V! s$ U E- {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]
0 p# M5 K2 h/ U8 V; _
. `) s% v& K0 s Z- z. u TThe 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-14.0 B1 @! u% ]1 Q
3 l* T+ P* c: ^9 [# _. K
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.2 Q' b6 K% j) b7 o' P) m) A
2 O, j! K0 u% K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 |
|