Hostname: page-component-78c5997874-t5tsf Total loading time: 0 Render date: 2024-11-15T23:22:39.313Z Has data issue: false hasContentIssue false

Augmentation of Indian Regional Navigation Satellite System to Improve Dilution of Precision

Published online by Cambridge University Press:  23 February 2010

Achanta D Sarma*
Affiliation:
(Osmania University, Hyderabad, India.)
Quddusa Sultana
Affiliation:
(Deccan College of Engineering and Technology, Hyderabad, India.)
Vemuri Satya Srinivas
Affiliation:
(Osmania University, Hyderabad, India.)
*

Abstract

The Indian Regional Navigation Satellite System (IRNSS) is an autonomous and independent navigational system being developed by India. IRNSS will provide position, navigation and timing services for national applications. To improve accuracy, it can be augmented using GPS and pseudolites (pseudo-satellites). In this paper, the effect on DOP (Dilution of Precision) due to augmentation of the proposed constellation of IRNSS with pseudolites is investigated. GDOP is reduced to 1·75 (max) from 3·63 (max) due to augmentation of IRNSS with two airport pseudolites (APLs). Due to augmentation of IRNSS with GPS, GDOP is reduced to 2·4 (max). When IRNSS is augmented with an APL as well as with GPS, GDOP is further decreased to 1·65 (max). The regional effect on DOP due to IRNSS is also investigated at different locations in the Indian region.

Type
Research Article
Copyright
Copyright © The Royal Institute of Navigation 2010

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

Singh, Arjun and Saraswati, (Nov. 2006). India Heads for a Regional Navigation Satellite System. Coordinates, a Magazine on Positioning and Navigation.Google Scholar
Cohen, C.E., Pervan, B.S., Cobb, H.S., Lawrence, D.G., Powell, J.D., and Parkinson, B.W (March 30–April 2, 1993). Real-Time Cycle Ambiguity Resolution using a Pseudolite for Precision Landing of Aircraft with GPS. DSNS '93, Amsterdam, The Netherlands.Google Scholar
DL-4plus User Manual (2005). Publication number: OM-20000063, Rev 6, printed in Canada. Novatel Inc.Google Scholar
Fukushima, S., Yoshihara, T., Suga, S. (2004). Evaluation of a Tropospheric Correction Model for Airport Pseudolite. Proceedings of 17th International Technical Meeting of the Satellite Division of the Institute of Navigation, Long Beach, CA.Google Scholar
Martin, S. (1999). Antenna Diagram Shaping for Pseudolite Transmitter Antennas – A solution to the Near-Far Problem. Proceedings of the 12th International Technical Meeting of the Satellite Division of the Institute of Navigation, Nashville, Tennessee.Google Scholar
Parkinson, W.B and Spilker, J.J (1996). Global Positioning System: Theory and Applications – vol. I and II. Institute of Aeronautics and Astronautics, Inc, Washington.Google Scholar
Suryanarayana, Rao K.N. (2007). Indian Regional Navigation Satellite System. IEEE Seminar on Global Satellite Navigation and Applications, Hyderabad, India.Google Scholar