Background1. Explain the principle of force gyroscopic stabilization Master gyrovertical ЦГВ is the gyrostabilized platform with two gyros based on the principle of force gyroscopic stabilization. It uses the normal erection system from liquid pendulum sensor and the quick erection system from mechanical pendulums for accelerated alignment of platform from tilts during pre-flight and in-flight procedures 2. What parameters influence the readiness time of master gyrovertical? The force gyroscopic stabilization is the control system in disturbance
It uses the normal erection system from liquid pendulum sensor and the quick erection system from mechanical pendulums for accelerated alignment of platform from tilts during pre-flight and in-flight procedures. Signals proportional to pitch and roll angles are output for all consumers from DC potentiometers. 3. Explain the operation of master gyro vertical in the stabilization mode Sensors are placed on the axes of gimbal mount where there are high disturbance moments which may cause the sufficient errors and even unbalance of gyrovertical 4. Explain the operation of master gyro vertical in the normal erection mode The master gyrovertical provides the signals of roll and pitch for large number of consumers. Sensors are placed on the axes of gimbal mount where there are high disturbance moments which may cause the sufficient errors and even unbalance of gyrovertical.
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