DocumentCode :
71384
Title :
Future Dual-Frequency GPS Navigation System for Intelligent Air Transportation Under Strong Ionospheric Scintillation
Author :
Jiwon Seo ; Walter, T.
Author_Institution :
Sch. of Integrated Technol., Yonsei Univ., Incheon, South Korea
Volume :
15
Issue :
5
fYear :
2014
fDate :
Oct. 2014
Firstpage :
2224
Lastpage :
2236
Abstract :
GPS technology is essential for future intelligent air transportation systems such as the Next Generation Air Transportation System (NextGen) of the United States. However, observed deep and frequent amplitude fading of GPS signals due to ionospheric scintillation can be a major concern in expanding GPS-guided aviation to the equatorial area where strong scintillation is expected. Current civil GPS airborne avionics track signals at a single frequency (L1 frequency) alone because it was the only civil signal available in the frequency band for aviation applications. The first GPS Block IIF satellite was launched in May 2010. This next-generation satellite transmits a new civil signal at the L5 frequency, which can be used for air transportation. This paper investigates a possible improvement in the availability of GPS-based aircraft landing guidance down to 200 ft above the runway, which is also known as Localizer Performance with Vertical Guidance (LPV) 200, under strong ionospheric scintillation when dual-frequency signals are available. Based on the availability study, this paper proposes and justifies a GPS aviation receiver performance standard mandating fast reacquisition after a very brief signal outage due to scintillation. In order to support a temporary single-frequency operation under a single-frequency loss due to scintillation, a new vertical protection level (VPL) equation is proposed and justified. With this new performance requirement and new VPL equation in place, 99% availability of LPV-200 would be attainable, rather than 50% at the current standards, even under the severe scintillation scenarios considered in this paper.
Keywords :
Global Positioning System; aircraft landing guidance; aircraft navigation; avionics; intelligent transportation systems; ionospheric electromagnetic wave propagation; radiowave propagation; signal processing; GPS Block IIF satellite; GPS aviation receiver performance standard; GPS signal tracking; GPS-based aircraft landing guidance; GPS-guided aviation; L1 frequency; L5 frequency; LPV 200; NextGen; VPL equation; amplitude fading; civil GPS airborne avionics; dual-frequency GPS navigation system; dual-frequency signals; intelligent air transportation systems; localizer performance with vertical guidance; next generation air transportation system; next-generation satellite; single-frequency loss; strong ionospheric scintillation; temporary single-frequency operation; vertical protection level; Availability; Correlation; Delays; Fading; Global Positioning System; Receivers; Satellites; Availability; dual-frequency global positioning system (GPS) aviation; intelligent air transportation; ionospheric scintillation;
fLanguage :
English
Journal_Title :
Intelligent Transportation Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
1524-9050
Type :
jour
DOI :
10.1109/TITS.2014.2311590
Filename :
6786014
Link To Document :
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