Abstract: | A new class of Ring Laser Gyro (RLG)-based strapdown inertial navigation systems has been established with the advent of Honeywell’s H-764G Integrated Embedded Global Positioning System/Inertial Navigation System (GPWNS). This system takes full advantage of precision pseudo-range and pseudo-range rate data available only from the embedded GPS receiver module which is integrated with the inertial data in a Kahnan filter. This synergistic approach results in superior operation in high dynamic, antenna shading, and jamming environments. As this paper will show, the H-764G successfully demonstrated this means of attaining the goal of low noise, precise navigation operation. Significant advantages exist in the embedded system mechanization when compared to the performance of stand-alone systems. Chief among these advantages is the outstanding performance obtained with fewer than four satellites in view; simplified installation; and reduced size, weight, and power. Through these distinctions, Honeywell has produced an embedded GPWINS that consistently demonstrates a more accurate navigation solution. This paper will serve to document the progressive development of the H-764G GPS/INS through a presentation of a brief system description, a look at the wide range of system applications, a review of a number of key discriminators. and finally, the exhibition of independently acquired test results from the Air Force’s Central Inertial Guidance Test Facility (CIGTF) and the Naval Research and Development division. |
Published in: |
Proceedings of the 1993 National Technical Meeting of The Institute of Navigation January 20 - 22, 1993 Parc 55 Hotel San Francisco, CA |
Pages: | 275 - 285 |
Cite this article: | Moya, David C., Elchynski, Joseph J., "Evaluation of the World's Smallest Integrated Embedded GPS/INS, the H-764G," Proceedings of the 1993 National Technical Meeting of The Institute of Navigation, San Francisco, CA, January 1993, pp. 275-285. |
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