TY - JOUR
T1 - Ionospheric Gradient Threat Mitigation in Future Dual Frequency GBAS
AU - Felux, Michael
AU - Circiu, Mihaela Simona
AU - Lee, Jiyun
AU - Holzapfel, Florian
N1 - Publisher Copyright:
© 2017 Michael Felux et al.
PY - 2017
Y1 - 2017
N2 - The Ground Based Augmentation System (GBAS) is a landing system for aircraft based on differential corrections for the signals of Global Navigation Satellite Systems (GNSS), such as GPS or Galileo. The main impact on the availability of current single frequency systems results from the necessary protection against ionospheric gradients. With the introduction of Galileo and the latest generation of GPS satellites, a second frequency is available for aeronautical navigation. Dual frequency methods allow forming of ionospheric free combinations of the signals, eliminating a large part of the ionospheric threats to GBAS. However, the combination of several signals increases the noise in the position solution and in the calculation of error bounds. We, therefore, developed a method to base positioning algorithms on single frequency measurements and use the second frequency only for monitoring purposes. In this paper, we describe a detailed derivation of the monitoring scheme and discuss its implications for the use in an aviation context.
AB - The Ground Based Augmentation System (GBAS) is a landing system for aircraft based on differential corrections for the signals of Global Navigation Satellite Systems (GNSS), such as GPS or Galileo. The main impact on the availability of current single frequency systems results from the necessary protection against ionospheric gradients. With the introduction of Galileo and the latest generation of GPS satellites, a second frequency is available for aeronautical navigation. Dual frequency methods allow forming of ionospheric free combinations of the signals, eliminating a large part of the ionospheric threats to GBAS. However, the combination of several signals increases the noise in the position solution and in the calculation of error bounds. We, therefore, developed a method to base positioning algorithms on single frequency measurements and use the second frequency only for monitoring purposes. In this paper, we describe a detailed derivation of the monitoring scheme and discuss its implications for the use in an aviation context.
UR - http://www.scopus.com/inward/record.url?scp=85017188493&partnerID=8YFLogxK
U2 - 10.1155/2017/4326018
DO - 10.1155/2017/4326018
M3 - Article
AN - SCOPUS:85017188493
SN - 1687-5966
VL - 2017
JO - International Journal of Aerospace Engineering
JF - International Journal of Aerospace Engineering
M1 - 4326018
ER -