|
本帖最后由 一身轻松 于 2013-10-16 23:45 编辑 0 L& z- G& E0 A& O
xlan1976 发表于 2013-10-16 23:30 8 W, @8 \ m& d6 C5 \8 [
。。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 ... / D' W, y8 E. i( D
& ~6 G) W+ i( k1 G/ eThe 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]# w6 y2 b S3 S" s9 A
* L, F3 Y/ ~7 e7 N( I1 ?8 u% u d% y
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.
$ L8 i3 _ L ^6 W4 A- X- t/ @% K/ t, |1 S! V
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.
: J" L# l) ^/ @3 G$ }! w
! ]5 U; f( K4 ~) t$ 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 |
|