Nick Seafort wrote:
I can only speak to spaceborne applications and therefore reaction wheels (as most spaceborne rate gyros are ring laser gyros now), but the primary causes of drift were most certainly a result of resistance in the mechanisms, and thermal effects. If it was purely a case of being "wound up" by the earth's rotation, then a spaceborne gyro would drift at a far higher rate - approximately 240 degrees per hour in low orbit! Luckily, those effects are easily static-calibrated out if predictable, and can even be dynamic-calibrated out to an extent if you have other types of sensors to compare against.
Inertial nav systems are integrated for the exact reason that no sensor is perfect, either in stability of measurement (jitter/random noise) or precision (the less precise, the greater the natural drift from reality). By combining different systems with clever filters, you can build a mostly self-correcting system with a long stability time before it starts to diverge significantly from reality, at which point you can reset it to a known calibration point and continue

The principle application of reaction wheels and giros on space craft is to control their movement not measure it. You can see how that works here on earth. When a motorcyclist turns left, for eg, he doesn't actually turn the handlebars left.
What he does is put a force that would turn the handlebars right which causes the gyroscopic effect of the front wheel to lean left, thereby changing the direction of travel for the motorbike to the left.
This is great in space because it doesn't require rocket fuel to point the spacecraft in a particular direction. A Control Moment Gyro is generally accepted as the most efficient way to do this due to a higher torque output for a given energy input when compared to reaction wheels and torque rods. The big disadvantage of CMG of course is gimbal lock and would require a backup system to continue operation.