Abstract: | With the onset of the first Special Category I (SCAT-I) Differential Global Navigation Satellite System (DGNSS) precision landing systems, and Category II and III systems to follow, several vendors are developing integrity algorithms to meet requirements. Meeting precision landing requirements involves trade- offs among four key requirements: accuracy, availability, integrity, and continuity. Simulation not only provides an excellent means for developing the appropriate design trade-offs, but also provides hardware-in-the-loop evaluation of precision approach ground system software during the software testing phase. This paper presents a discussion on the testing of integrity algorithms using simulation. |
Published in: |
Proceedings of the 9th International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GPS 1996) September 17 - 20, 1996 Kansas City, MO |
Pages: | 1671 - 1675 |
Cite this article: | Cole, Reggie, "Simulation Testing of Precision Approach Integrity Algorithms," Proceedings of the 9th International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GPS 1996), Kansas City, MO, September 1996, pp. 1671-1675. |
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