ORIGINAL: erbroens
Yes, the F-16 was the first combat jet in the world with negative static stability built in corrected by gyros and a computer and with a fly by wire system.. all this for making this plane extremely agile.
Of course, the computer of this airplane has a set of "flight rules" that takes data from its sensors (airspeed, rotational, acceleration,air density, etc) for stabilizing it. A simple sense rate gyro like we have available wouldn´t work as well as we need.
Just to see how complex is this, take a look in this video of a test flight of a F-16 with a assimetric ordenance issue to be resolved.
http://www.youtube.com/watch?v=Rv9YC-gaNYo
Hey Guys:
Watch this:
http://www.aerosoft2.de/downloads/f1...l_F16_Engl.pdf
Page 12 of 50 "Relaxed Stability"
At Mach 1.0, the lift will be at the same point of C.G. Above Mach 1.0, the lift will be behid C.G. This means that F-16 is aerodynamically stable above Mach 1.0
Below Mach 1.0, the F-16is aerodynamically unstable.