The paper compares and describes the advantages of dry tuned gyros over floated gyros for space applications. Attention is given to describing the Teledyne SDG-5 gyro and the second-generation NASA Standard Dry Rotor Inertial Reference Unit (DRIRU II). Certain tests which were conducted to evaluate the SDG-5 and DRIRU II for specific mission requirements are outlined, and their results are compared with published test results on other gyro types. Performance advantages are highlighted.
Performance advantages of dynamically tuned gyroscopes in high accuracy spacecraft pointing and stabilization applications
Symposium on Gyro Technology
01.01.1979
Sonstige
Keine Angabe
Englisch
Galileo spacecraft pointing accuracy analysis
NTRS | 1982
|Galileo spacecraft pointing accuracy analysis
AIAA | 1982
|