Hostname: page-component-76fb5796d-x4r87 Total loading time: 0 Render date: 2024-04-28T19:57:16.431Z Has data issue: false hasContentIssue false
  • English
  • Français

Inertia Navigation Systems

Published online by Cambridge University Press:  18 January 2010

E. W. Anderson
E. W. Anderson
Affiliation:
(Sperry Gyroscope Company)
Get access Rights & Permissions [Opens in a new window]

Extract

The object of this paper is to present various practical solutions to the problems of inertia navigation in a descriptive rather than a mathematical form. Inertia navigation is an automatic bump of locality, a dead-reckoning device which, starting from a known point, seeks to find position. Other dead-reckoning devices measure speed, which is only relative to the fluid sea or air. Inertia navigation measures accelerations, which are absolute, and hence builds up a measure of speed. The accelerometer is, therefore, a good starting point for our survey.

Type
Research Article
Information
The Journal of Navigation , Volume 11 , Issue 3 , July 1958 , pp. 231 - 258
Copyright
Copyright © The Royal Institute of Navigation 1958

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

1Adams, D. E. (1956). Introduction to inertial navigation. This Journal, 9, 249.Google Scholar
2Cawood, W. (1957). Some design problems in inertia navigation. (Office Nationale d'Éudes et de Recherche Aeronautiques, Paris.)Google Scholar
3Holahan, J. (1957). Three approaches to inertial system design, Aviation Age, Nov. 1957.Google Scholar
4Klass, P. J. (1956). Inertial navigation, Aviation Week, nos. 1–4.Google Scholar