|
本帖最后由 一身轻松 于 2013-10-16 23:45 编辑 ?9 P* s% O X( B& |# m7 \
xlan1976 发表于 2013-10-16 23:30 ![]()
3 N2 G! t- @+ t3 }: s: a( c。。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 ...
" p# ]' i6 y, R4 h! q
; {0 T* e' X) t" G0 W+ E# a4 Z, ~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]
1 c! f) y8 U% ]. A; D- N. u3 ^
, K/ {7 G' p/ m( z( LThe 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.- v$ l" C( n0 A# A
3 i e3 q3 O: U' z7 x
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.9 |6 p9 |, I8 `
& V0 E+ P. ]9 d8 o6 B4 K. ^/ B
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 |
|