TY - JOUR
T1 - Baseline-constrained single-epoch GNSS attitude determination using a priori attitude information
AU - SUN, Xiucong
AU - WANG, Yuan
AU - JIANG, Yiping
AU - BAI, Shengzhou
N1 - Publisher Copyright:
© 2024 The Authors
PY - 2025/8
Y1 - 2025/8
N2 - Instantaneous Global Navigation Satellite System (GNSS) attitude determination method which achieves real-time attitude determination using GNSS signal has been extensively studied, particularly the one using a priori attitude information replacing the code measurements to enhance the successful rate for ambiguity resolution. However, there exists a key limitation that this method relies on considerable Monte Carlo sampling particles to construct the pdf of ambiguities, resulting in significant computational burdens. To address this limitation, this paper provides a rapid single-epoch GNSS attitude determination method based on a priori attitude information. It utilizes a second-order Taylor expansion to analytically estimate the covariance of the baseline conditioned on a priori attitude information. This is followed by deriving the float solution and covariance of ambiguities, which are then processed using the standard LAMBDA method for integer ambiguity resolution. Experimental results demonstrate that our method is both efficient and accurate, significantly reducing computational costs compared to previous methods, thereby enhancing its applicability for GNSS-based attitude determination.
AB - Instantaneous Global Navigation Satellite System (GNSS) attitude determination method which achieves real-time attitude determination using GNSS signal has been extensively studied, particularly the one using a priori attitude information replacing the code measurements to enhance the successful rate for ambiguity resolution. However, there exists a key limitation that this method relies on considerable Monte Carlo sampling particles to construct the pdf of ambiguities, resulting in significant computational burdens. To address this limitation, this paper provides a rapid single-epoch GNSS attitude determination method based on a priori attitude information. It utilizes a second-order Taylor expansion to analytically estimate the covariance of the baseline conditioned on a priori attitude information. This is followed by deriving the float solution and covariance of ambiguities, which are then processed using the standard LAMBDA method for integer ambiguity resolution. Experimental results demonstrate that our method is both efficient and accurate, significantly reducing computational costs compared to previous methods, thereby enhancing its applicability for GNSS-based attitude determination.
KW - Aerospace engineering
KW - Ambiguity resolution
KW - GNSS
KW - Instantaneous attitude determination
KW - Navigation systems
KW - Satellites
UR - https://www.scopus.com/pages/publications/105009622215
U2 - 10.1016/j.cja.2024.11.031
DO - 10.1016/j.cja.2024.11.031
M3 - 文章
AN - SCOPUS:105009622215
SN - 1000-9361
VL - 38
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 8
M1 - 103321
ER -