Planes determine altitude and speed from air pressure readings. But near the speed of sound, things become very nonlinear. As fighter planes became supersonic in the 1950s, the CADC was built to compute these nonlinear functions using rotations of gears and cams.
The CADC needs to know the temperature for its calculations. A platinum probe outside the plane measures temperature, producing a changing resistance. But the CADC needs to rotate gears. How does the CADC convert the resistance to a rotation? That's what I'll discuss today.