IT is readily understood that no instrument or measuring device can be entirely free from errors duo to physical imperfections of manufacture. Gyroscopes in particular are affected in this way, requiring, as they do, complete absence of bearing friction if use is to be made of their property of preserving fixity in space of the direction of their spin axis when free from external forces. The impossibility of achieving this ideal condition results in a small degree of drift of the gyro‐axis, and detracts from the value of a gyroscope as a direction indicating device. In spite of this deficiency, in cases where steadiness of pointer reading is of prime importance, standard gyroscopic directional instruments serve a very useful purpose, provided the necessity of applying corrections at appropriate time intervals is recognized and observed. Latterly, development along the lines of automatic compensation has overcome this defect, and has led to the advent of the ‘monitored’ gyroscopic compass.
Article navigation
Review Article|
January 01 1948
Turning Errors of a Monitored Directional Gyroscope: A General Statement of the Nature and Magnitude During the Course of, and Immediately after Recovery from, a True Banked Horizontal Turn and the Influence of Residual Compass Error on the A.P.I.
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1948
Aircraft Engineering (1948) 20 (1): 11–17.
Citation
Price H (1948), "Turning Errors of a Monitored Directional Gyroscope: A General Statement of the Nature and Magnitude During the Course of, and Immediately after Recovery from, a True Banked Horizontal Turn and the Influence of Residual Compass Error on the A.P.I.". Aircraft Engineering, Vol. 20 No. 1 pp. 11–17, doi: https://doi.org/10.1108/eb031589
Download citation file:
189
Views
New and popular articles
Suggested Reading
Turning Errors of a Monitored Directional Gyroscope
Aircraft Engineering (February,1948)
Micromachined gyroscopic sensors
Sensor Review (March,1999)
Auxiliary Equipment
Aircraft Engineering (August,1958)
Vibrating structure gyroscopes
Sensor Review (March,1996)
Influence of weak and strong gyroscopic effects on light aircraft dynamics
Aircraft Engineering and Aerospace Technology: An International Journal (September,2016)
Related Chapters
CHAPTER VII. METHODS OF OBSERVING THE ROLLING.AND PITCHING MOTIONS OF SHIPS.
A manual of naval architecture, for use of officers of the Royal Navy, officers of the mercantile marine, yachtsmen, shipowners, and shipbuilders
Strain monitoring and analysis of a steel pipe during horizontal directional crossing
Transforming the Future of Infrastructure through Smarter Information: Proceedings of the International Conference on Smart Infrastructure and ConstructionConstruction, 27–29 June 2016
Smartphones equipped with android application software for structural health monitoring
Transforming the Future of Infrastructure through Smarter Information: Proceedings of the International Conference on Smart Infrastructure and ConstructionConstruction, 27–29 June 2016
Recommended for you
These recommendations are informed by your reading behaviors and indicated interests.
