Hostname: page-component-586b7cd67f-gb8f7 Total loading time: 0 Render date: 2024-11-28T15:18:33.919Z Has data issue: false hasContentIssue false
  • English
  • Français

Integration of Satellite and Inertial Positioning Systems

Published online by Cambridge University Press:  21 October 2009

M. Napier
M. Napier
Affiliation:
(Institute of Engineering Surveying and Space Geodesy, University of Nottingham)
Get access Rights & Permissions [Opens in a new window]

Extract

The Global Positioning System (GPS) offers an absolute positioning accuracy of 15 to 100 metres. Inertial navigation complements GPS in that it provides relative positioning and is totally self-contained. These two positioning sensors are ideally suited for system integration for although there is not necessarily an improvement in accuracy, the integration of GPS with inertial navigation systems (INS) does enable an increase in system performance.

Type
Research Article
Information
The Journal of Navigation , Volume 43 , Issue 1 , January 1990 , pp. 48 - 57
Copyright
Copyright © The Royal Institute of Navigation 1990

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

1Diesel, J. W. (1987). Integration of GPS/INS for maximum velocity accuracy. Navigation, Vol. 34, No. 3.CrossRefGoogle Scholar
2Rounds, S. F. (1987). A fully integrated GPS/Doppler/Inertial navigation system. Proceedings of the Satellite Division First Technical Meeting, Colorado Springs, 21–25 September, 1987.Google Scholar
3Du Hart III, J. H. and Semler, J. R. (1987). An integrated Gps/strapdown inertal navigator postmission processor and initial test results. Proceedings of the Satellite Division First Technical Meeting, Colorado Springs.Google Scholar
4Knight, D. T. (1987). GPS integration with low-cost inertial navigation unit. Proceedings of the Satellite Division First Technical Meeting, Colorado Springs.Google Scholar
5Frazier, D. E.et al. (1987). T-33 Aircraft demonstration of cps/aided inertial navigation. Proceedings of the Satellite Division First Technical Meeting, Colorado Springs.Google Scholar
6Hartman, R. G. (1987). An integrated GPS/IRS design approach. Proceedings of the Satellite Division First Technical Meeting, Colorado Springs.Google Scholar
7Aggarwal, A. K. (1987). Integration of differential GPS with INS for precise position, attitude and azimuth determination. Proceedings of the Satellite Division First Technical Meeting, Colorado Springs.Google Scholar
8Ashkenazi, V. (1989). Positioning by satellites; Principles, achievements and prospects. Proceedings of NAV 89 - Satellite Navigation, the 1989 International Conference of the Royal Institute of Navigation, London.Google Scholar
9Napier, M. E. (1987). Kalman filter algorithms. Lecture notes for a seminar on ‘Kalman Filtering’, Department of Civil Engineering, University of Nottingham, February 1987.Google Scholar
10Gelb, A. (1974). Applied Optimal Estimation. Cambridge, MA: M.I.T. Press.Google Scholar
11Bierman, J. (1977). Factorization Methods for Discrete Sequential Estimation. New York: Academic Press.Google Scholar
12Tazartes, D. A. and Mark, J. G. (1988). Integration of GPS receivers into existing navigation systems. Navigation, Vol. 35, No. 1.CrossRefGoogle Scholar