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Open Access

Baseline-constrained single-epoch GNSS attitude determination using a priori attitude information

Xiucong SUNaYuan WANGaYiping JIANGb( )Shengzhou BAIb
School of Aeronautics, Beihang University, 100191 Beijing, China
Department of Aeronutical and Avition Engineering, Hong Kong Polytechnic University, 999077 Hong Kong, China

Special Issue: GNSS Technology and Application.

Peer review under responsibility of Editorial Committee of CJA

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Abstract

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.

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Chinese Journal of Aeronautics

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Cite this article:
SUN X, WANG Y, JIANG Y, et al. Baseline-constrained single-epoch GNSS attitude determination using a priori attitude information. Chinese Journal of Aeronautics, 2025, 38(8). https://doi.org/10.1016/j.cja.2024.11.031

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Received: 01 July 2024
Revised: 02 August 2024
Accepted: 09 October 2024
Published: 02 December 2024
© 2024 The Authors. Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).