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首页> 外文期刊>IEEE Transactions on Aerospace and Electronic Systems >Low-Complexity Instantaneous Ambiguity Resolution with the Affine-Constrained GNSS Attitude Model
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Low-Complexity Instantaneous Ambiguity Resolution with the Affine-Constrained GNSS Attitude Model

机译:仿射约束的GNSS姿态模型的低复杂度瞬时歧义解析

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摘要

In this contribution a new approach to ambiguity resolution for Global Navigation Satellite System (GNSS)-based attitude estimation applications is discussed and tested. This approach enhances the observation model by means of additional linear constraints. These constraints are implicitly derived by applying an affine transformation to the unknown real-valued parameters, and largely aid the integer ambiguity estimation through an improved float estimation. The new method is characterized by a lower computational complexity than a rigorous nonlinearly-constrained GNSS attitude model, and at the same time it guarantees higher performance than unconstrained, and therefore weaker, models. The ambiguity resolution performance of the affine-constrained approach is tested through a series of simulated as well as actual data sets, demonstrating the validity and usefulness of the proposed approach for multi-antenna GNSS-based attitude determination applications.
机译:在这项贡献中,讨论并测试了一种新的基于全球导航卫星系统(GNSS)的姿态估计应用中的歧义解决方法。这种方法通过附加的线性约束来增强观察模型。这些约束是通过对未知的实值参数应用仿射变换来隐式导出的,并且通过改进的浮点估计在很大程度上有助于整数歧义估计。与严格的非线性约束GNSS姿态模型相比,该新方法的特点是计算复杂度低,并且与无约束模型(因此较弱)相比,它可以保证更高的性能。通过一系列模拟和实际数据集来测试仿射约束方法的歧义分辨率性能,证明了该方法在基于多天线GNSS的姿态确定应用中的有效性和实用性。

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