DocumentCode :
2056228
Title :
Tightly coupled GPS/IRS navigation for ADS-B
Author :
Manfred, Mark ; Ryno, Thomas
Author_Institution :
Honeywell Int., Minneapolis, MN
fYear :
2008
fDate :
5-7 May 2008
Firstpage :
1
Lastpage :
7
Abstract :
The FAA has proposed challenging requirements for the ADS-B navigation sensor FAA´s recent Notice of Proposed Rulemaking (NPRM) for ADS-B concludes WAAS meets the proposed requirements but says the FAA is considering whether tightly coupled GNSS/IRS navigation is an acceptable alternative. Navigation systems that tightly integrate GPS with an Inertial Reference System (IRS) are indeed an excellent positioning source for ADS-B. Air transport and business aircraft are beginning to use such systems for a variety of reasons unrelated to ADS-B, for example to improve availability for RNP 0.1 operations. This trend will accelerate over the coming decade. This paper describes tightly coupled GPS/IRS navigation systems and the benefits they provide. It shows they not only meet the ADS-B NPRM requirements for horizontal positioning, but they also offer several additional benefits that enhance ADS-B´s capability to maintain air traffic flow under challenging conditions that would otherwise impede it.
Keywords :
Global Positioning System; air traffic control; aircraft instrumentation; aircraft navigation; inertial navigation; ADS-B navigation sensor; FAA; Global Positioning System; air traffic flow maintenance; air transport; business aircraft; horizontal positioning; inertial reference system; tightly coupled GPS/IRS navigation; Acceleration; Aircraft navigation; Business; FAA; Filters; Flexible manufacturing systems; Global Positioning System; Heart; Impedance; Satellite navigation systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Integrated Communications, Navigation and Surveillance Conference, 2008. ICNS 2008
Conference_Location :
Bethesda, MD
Print_ISBN :
978-1-4244-2303-3
Electronic_ISBN :
978-1-4244-2304-0
Type :
conf
DOI :
10.1109/ICNSURV.2008.4559165
Filename :
4559165
Link To Document :
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