基于约束包裹最小二乘方法的GNSS姿态确定

Xing Liu, Tarig Ballal, T. Al-Naffouri
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引用次数: 3

摘要

基于全球导航卫星系统(GNSS)的姿态确定已成为传统技术的重要替代方案。载波相位整数模糊度的解决是高精度GNSS姿态确定的主要挑战。在这篇论文中,我们创新地开发了一种约束包裹最小二乘(C-WLS)方法来估计车辆的姿态。该方法通过求解空间的搜索过程,直接利用模糊的载波相位观测来确定飞行器的姿态,避免了求解整数模糊的复杂过程。该方法还利用了一种新的优化模型,该模型利用了天线配置、载波相位模糊度的整数特性以及载波相位观测的噪声分布等先验信息。仿真和实验数据验证了该方法的有效性。结果表明,本文提出的C-WLS方法在各个性能领域都优于著名的约束LAMBDA方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
GNSS Attitude Determination Using a Constrained Wrapped Least Squares Approach
Global Navigation Satellite Systems (GNSS) based attitude determination has become an essential alternative to conventional techniques. carrier-phase integer ambiguity resolution is the primary challenge for high-precision GNSS attitude determination. In this contribution, we develop a constrained wrapped least squares (C-WLS) method to estimate a vehicle's attitude innovatively. The proposed method avoids the complicated process of resolving integer ambiguities by directly employing ambiguous carrier-phase observations to determine a vehicle's attitude through a search procedure in the solution space. The proposed method also takes advantage of a novel optimization model, which leverages prior information such as antenna configuration, the integer property of the carrier-phase ambiguity, and the noise distribution of carrier-phase observations. The performance of the proposed method is verified using both simulation and experimental data. The results show that the proposed C-WLS method outperforms the renowned constrained LAMBDA method in various performance areas.
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