Where are electrical signals from the rate gyro continuously supplied to compensate for attitude changes?

The rate gyro is a critical component in aviation and aerospace systems, primarily used for sensing changes in orientation or attitude. It provides continuous electrical signals that reflect the aircraft's angular rate of motion. These signals are vital for compensating for attitude changes to maintain stability and control during flight.

Radar antenna stabilization circuits specifically rely on these signals to adjust the antenna's position in response to the aircraft's movements. This ensures that the radar system can maintain a stable reference point for tracking targets or maintaining a clear communication line, despite the aircraft's maneuvers and changes in orientation. By continually processing the electrical signals from the rate gyro, these circuits can proactively adjust the radar system, enhancing performance and accuracy.

In contrast, while flight control systems do utilize information from rate gyros, their primary focus is on broader control mechanisms rather than stabilization of specific equipment like radar antennas. Navigation displays may show the aircraft's attitude but do not utilize the gyro signals in a way that compensates for attitude changes directly. Ground control stations are involved in broader communication and operational aspects rather than real-time compensation for aircraft attitude changes.