|
本帖最后由 一身轻松 于 2013-10-16 23:45 编辑
8 d% V$ H; `: g/ kxlan1976 发表于 2013-10-16 23:30 ![]()
( M* Y; Q& [. H( ]; g6 F- \。。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 ... 9 |! `6 p; V1 Z) T# r' H( {2 A
" ~1 h0 X5 {8 t% 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]' ~' z! l. L }: q
- v% E1 N! _" ]8 ]
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.
! l" c5 z3 q( w% d$ L- s" b' l7 i1 c$ c$ I8 {: V: D
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.7 q$ L) @6 g& S) P1 F- m5 A
2 `. P# E" K- E$ {2 V) k* f! m
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 |
|