Hostname: page-component-cd9895bd7-mkpzs Total loading time: 0 Render date: 2024-12-27T10:14:52.410Z Has data issue: false hasContentIssue false
  • English
  • Français

Current Status of Flight Evaluation of DGPS-INS Hybrid Navigation System at NAL*

Published online by Cambridge University Press:  21 October 2009

H. Shingu ,
M. Murata ,
T. Ono  and
K. Ishikawa
H. Shingu
Affiliation:
(National Aerospace Laboratory, Tokyo)
M. Murata
Affiliation:
(National Aerospace Laboratory, Tokyo)
T. Ono
Affiliation:
(National Aerospace Laboratory, Tokyo)
K. Ishikawa
Affiliation:
(National Aerospace Laboratory, Tokyo)
Get access Rights & Permissions [Opens in a new window]

Abstract

This paper presents a summary of the flight evaluation of the DGPS-INS hybrid navigation system conducted at the National Aerospace Laboratory (NAL). First, the configuration of the flight experiments, including ground facilities, the measurement system, etc. is described. Secondly, the design concept for a method of estimating navigation errors using a Kalman filter is presented. Thirdly, flight profiles employed in the experiments are defined, and the experimental results of GPS, DGPS, INS, in both stand-alone and hybrid modes are shown corresponding to each profile, and the improvement of navigation performance by the introduction of the DGPS-INS hybrid navigation system is experimentally verified. Fourthly, the future plan for research on the DGPS-INS hybrid navigation system at NAL is briefly explained. Finally, it is concluded that the design concept of the DGPS-INS hybrid navigation system available for future space vehicles has been successfully completed.

Keywords

1. Satellite navigation.2. Inertial systems.3. Integrated systems.4. Terminal area navigation.
Type
Research Article
Information
The Journal of Navigation , Volume 47 , Issue 3 , September 1994 , pp. 338 - 348
Copyright
Copyright © The Royal Institute of Navigation 1994

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

1Kruczysky, L. R. (1977). Global Positioning System Navigation Algorithms, Applied Mechanics Research Laboratory, University of Texas, Austin.Google Scholar
2Gregory, T. K. et al. (1990). The effect of Selective Availability on differential GPS corrections, Journal of the US Institute of Navigation, 37, (1).Google Scholar
3Murata, M. and Harigae, M. (1992). The observations and analysis of Selective Availability in GPS, Transactions of the Society of Instrument and Control Engineers, 28, (1), pp. 40∼49. (in Japanese).CrossRefGoogle Scholar
4Jacob, T. (1989). Integrated flight guidance system using differential-GPS for landing approach guidance. AGARD CP455, pp. 25–1 ~ 25–10.Google Scholar
5Ono, T. et al. (1994). A preliminary evaluation test of GPS / DGPS navigation system. Technical Papers, International Pacific Air & Space Technology Conference, Feb. 1994.CrossRefGoogle Scholar
6Shingu, H. et al. (1992). Flight evaluation of DGPS and DGPS-INS navigation systems. Proceedings of the 18th International Symposium on Space Technology and Science, pp. 1115∼1123, May 1992.Google Scholar
7Murata, M. et al. (1992). A GPS surveying method applied to approach/landing navigation flight experiments. Journal of the Geodetic Society of Japan, 38, (2), pp. 137∼149.Google Scholar