Detailed derivation of the transfer function for a multigimbal, elastically supported, tuned gyro is presented and comparison made between its characteristics and those of a classical two-axis, free-rotor gyro. Knowledge of the gyro transfer function is necessary for the purpose of servo analysis of the system in which the gyro is used; also, the transfer function is a basis of evaluation of errors caused by angular inputs that occur at twice spin frequency.
Theory of Operation of an Elastically Supported Tuned Gyroscope
IEEE Transactions on Aerospace and Electronic Systems ; AES-8 , 3 ; 280-288
1972-05-01
2293177 byte
Article (Journal)
Electronic Resource
English
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