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Inertial Attitude Sensor Unit Consisted of Four Rate Integrating Gyros
Pages: 25-28+12
Year: Issue:  3
Journal: Aerospace Control

Keyword:  Attitude controlAngular rate gyroscopeIntegrating gyroscope;
Abstract: This paper presents a inertial attitude sensor unit consisted of four floated rate in-tegrating gyros for sensing satellite three--axis attitudes, gives its implementation scheme,principle of angular rate measurement and reliability analysis, and demonstrates that its is aeffective, economic,feasible scheme.
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