Abstract
In the BDS-3 constellation, only the B3I signal is used to compute the broadcast clock offset. However, because advanced receiver autonomous integrity monitoring (ARAIM) uses dual-frequency measurements, the time group delay (TGD) must be considered in BDS-3-based ARAIM applications. The existing BDS-3 error model is therefore not sufficient to describe the actual TGD error encountered by aviation users. Specifically, the estimated signal-in-space error underestimates the actual error, which cannot be bounded by the estimated user range accuracy and nominal bias. This inaccuracy results in a loss of integrity. To avoid this risk, this paper develops a separated Gaussian model to bound the TGD error for BDS-3 in ARAIM. Using a one-year data set, this paper char-acterizes and bounds the TGD error for different signal combinations. Of the tested combinations, the B1C/B2a signal combination resulted in the smallest standard deviation of 0.78 m and a corresponding bias component of 0.71 m. We suggest that this signal combination be adopted for use in ARAIM.
| Original language | English |
|---|---|
| Article number | navi.705 |
| Journal | Navigation, Journal of the Institute of Navigation |
| Volume | 72 |
| Issue number | 3 |
| DOIs | |
| Publication status | Published - 1 Sept 2025 |
Keywords
- ARAIM
- BDS-3
- integrity
- time group delay
ASJC Scopus subject areas
- Aerospace Engineering
- Electrical and Electronic Engineering
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