Title :
An Automatic Gyro Mass-Unbalance Measuring Technique
Author_Institution :
Inertial Navigation, Autonetics Division, North American Aviation, Inc., Downey, Calif.
Abstract :
An inertial navigation system containing a versatile computer can be given the capability of automatically measuring its gyro mass unbalance. These measurements are accomplished in tests performed and monitored by the computer. Mass-unbalanced drifts induced by tilting the stable platform are detected by the system´s acceleration sensors. From the outputs of these sensors, the computer determines the mass-unbalance components using regression-analysis techniques that minimize errors of extraneous origin.
Keywords :
Acceleration; Computerized monitoring; Control systems; Equations; Inertial navigation; Military computing; Performance evaluation; Sensor systems; Test equipment; Testing;
Journal_Title :
Military Electronics, IEEE Transactions on
DOI :
10.1109/TME.1963.4323039