2016 IEEE Aerospace Conference 2016
DOI: 10.1109/aero.2016.7500884
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Ionospheric monitoring in a dual frequency GBAS

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Cited by 5 publications
(7 citation statements)
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“…Based on the available single frequency corrections (L1/E1 and L5/E5a) Ifree corrections can be formed on the airborne side. In order to remove the ionospheric delay the single frequency corrections have to be generated using the same smoothing time constant [10].…”
Section: 2mentioning
confidence: 99%
“…Based on the available single frequency corrections (L1/E1 and L5/E5a) Ifree corrections can be formed on the airborne side. In order to remove the ionospheric delay the single frequency corrections have to be generated using the same smoothing time constant [10].…”
Section: 2mentioning
confidence: 99%
“…In this way, ionospheric delays affecting both the ground and the aircraft are estimated by the airborne subsystem using a quantity called pseudo ionospheric delay. The details about this monitoring strategy are found in Felux et al (2016;. Note that each aircraft is required to make its own ionospheric integrity determination because, while it obtains pseudorange corrections from the ground, it has no means to provide its measurements or delay estimates back to the ground station (i.e., the GBAS VDB only communicates information in one direction, from ground to aircraft).…”
Section: Dual-frequency Multi-constellation Gbasmentioning
confidence: 99%
“…The largest portion of this will be the receiver clock but it also includes the part of the ionospheric delay that is common to all satellites. For that reason, only the information about the difference in the ionospheric delay between the satellites is contained in the corrections [5].…”
Section: Dual Frequency Monitoringmentioning
confidence: 99%
“…In order to decide now if the difference of the observations from the ground and airborne system poses a threat to the airborne user or not a threshold for this monitor is necessary. In [5] we derived the monitoring threshold based on the airworthiness requirements as given in the CS-AWO [8] and the AC-120 28B [9]. The derivation uses the requirement to land within the touchdown box on the runway.…”
Section: Dual Frequency Monitoringmentioning
confidence: 99%
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