Transient performance of a single-axis rate gyroscope mounted in a spacecraft which is spinning about the spin axis of the gyro is presented. Analytical expressions for various time-domain and frequency-domain specifications as functions of the spin rate of the vehicle are obtained. Numerical results are presented which are useful in selecting the gyro parameters if it is to be used for the measurement of the angular velocity in spinning space vehicles.
Transient performance of gyro in spinning spacecraft
Transientes Verhalten eines Gyroskops in einem rotierenden Raumfahrzeug
IEEE Transactions on Aerospace and Electronic Systems ; AES-23 , 5 ; 620-624
1987
5 Seiten, 10 Quellen
Article (Journal)
English
Transient Performance of Gyro in Spinning Spacecraft
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