DAMPING OF THE TORSION STEM OF A TUNING FORK GYROSCOPE
Abstract
The Coriolis Torques produced by the application of a rate of turn to a tuning-fork gyroscope are measured by the response of a tuned torsion stem. Methods of damping the motion of this stem and the optimum magnitude of this damping are examined theoretically.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1962
- Accession Number
- AD0343756
Entities
People
- G. H. Hunt
Organizations
- Royal Aircraft Establishment