TY - GEN
T1 - Impact of tropospheric anomalies on GBAS integrity
AU - Zhuang, Yuanyuan
AU - Wang, Zhipeng
AU - Fang, Kun
AU - Zhu, Yanbo
N1 - Publisher Copyright:
© 2020 ION 2020 International Technical Meeting Proceedings. All rights reserved.
PY - 2020
Y1 - 2020
N2 - Ground-based augmentation systems (GBAS) improve the positioning accuracy of aircraft through differential correction techniques during the approach process and enable aircraft to achieve higher services through various monitoring algorithms. Many errors need to be eliminated during navigation. Tropospheric delay is one of the most critical errors in a GBAS. Under normal atmospheric conditions, most of the tropospheric delays can be eliminated by using the difference method and TC model. However, these methods are not applicable under anomalous atmospheric conditions, and abnormal atmospheric conditions have been observed by both the International Civil Aviation Organization (ICAO) and Single European Sky Air Traffic Management Research (SESAR). Anomalous atmospheric conditions pose a great threat to aircraft safety. An integrity monitoring approach may be taken, or the threat may be incorporated into the normal model and overbounded by the protection levels. This paper focuses on non-nominal anomalies in different regions and in different seasons. We found that the maximum residual tropospheric delay caused by non-nominal anomalies exceeds 35 cm. In addition, the frequency of and the maximum residual tropospheric delay caused by the simultaneous occurrence of duct anomalies and non-nominal anomalies are studied here. We found that the maximum frequency of non-nominal and duct anomalies occurring simultaneously exceeds 70%. Finally, this paper used the previously developed overbound method to overbound the two kinds of tropospheric anomalies using data from Dongying Airport. We found that the impact of duct anomalies on the protection levels is greater than that of non-nominal anomalies at Dongying Airport.
AB - Ground-based augmentation systems (GBAS) improve the positioning accuracy of aircraft through differential correction techniques during the approach process and enable aircraft to achieve higher services through various monitoring algorithms. Many errors need to be eliminated during navigation. Tropospheric delay is one of the most critical errors in a GBAS. Under normal atmospheric conditions, most of the tropospheric delays can be eliminated by using the difference method and TC model. However, these methods are not applicable under anomalous atmospheric conditions, and abnormal atmospheric conditions have been observed by both the International Civil Aviation Organization (ICAO) and Single European Sky Air Traffic Management Research (SESAR). Anomalous atmospheric conditions pose a great threat to aircraft safety. An integrity monitoring approach may be taken, or the threat may be incorporated into the normal model and overbounded by the protection levels. This paper focuses on non-nominal anomalies in different regions and in different seasons. We found that the maximum residual tropospheric delay caused by non-nominal anomalies exceeds 35 cm. In addition, the frequency of and the maximum residual tropospheric delay caused by the simultaneous occurrence of duct anomalies and non-nominal anomalies are studied here. We found that the maximum frequency of non-nominal and duct anomalies occurring simultaneously exceeds 70%. Finally, this paper used the previously developed overbound method to overbound the two kinds of tropospheric anomalies using data from Dongying Airport. We found that the impact of duct anomalies on the protection levels is greater than that of non-nominal anomalies at Dongying Airport.
UR - https://www.scopus.com/pages/publications/85082455556
U2 - 10.33012/2020.17189
DO - 10.33012/2020.17189
M3 - 会议稿件
AN - SCOPUS:85082455556
T3 - ION 2020 International Technical Meeting Proceedings
SP - 944
EP - 963
BT - ION 2020 International Technical Meeting Proceedings
PB - Institute of Navigation
T2 - Institute of Navigation International Technical Meeting 2020, ITM 2020
Y2 - 21 January 2020 through 24 January 2020
ER -