一种GNSS双天线测向自适应卫星筛选算法

By using a GNSS dual-antenna direction finding adaptive satellite selection algorithm, dynamically adjusting the elevation angle and carrier-to-noise ratio threshold, and combining multi-dimensional scoring and heading accuracy evaluation, the contradiction between satellite quality and quantity in complex environments of the GNSS dual-antenna direction finding system is resolved, achieving high-precision and continuous heading angle calculation.

CN120630252BActive Publication Date: 2026-07-17XIAMEN XINNUO TECH

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
XIAMEN XINNUO TECH
Filing Date
2025-07-25
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing GNSS dual-antenna direction finding systems struggle to balance the conflict between satellite quality and quantity in complex environments, resulting in limited direction finding accuracy and continuity. In particular, redundancy decreases in open scenarios, or insufficient satellite numbers lead to system failure in obstructed scenarios.

Method used

An adaptive satellite selection algorithm for GNSS dual-antenna direction finding is adopted. By constructing an environmental state vector, the elevation angle and carrier-to-noise ratio threshold are dynamically adjusted. Combined with a multi-dimensional satellite comprehensive scoring function and a heading accuracy evaluation function, the optimal set of satellites is selected. Furthermore, the ambiguity resolution is optimized by baseline length and condition number constraints, thereby improving the robustness and accuracy of the system.

Benefits of technology

It significantly improves the accuracy and stability of heading angle in complex environments, ensuring that the system continuously outputs high-precision heading information in different scenarios, reducing computational load and enhancing the system's adaptability and anti-interference capabilities.

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Abstract

本发明提供了一种GNSS双天线测向自适应卫星筛选算法,本发明涉及卫星导航技术领域,本发明通过初始化高度角与载噪比门限完成首轮可见卫星筛选,随后以卫星数量、平均载噪比、载噪比标准差及平均高度角构建环境状态向量,驱动自适应函数实时重设门限,确保复杂场景下卫星可用性。多维度综合评分函数进一步剔除低质量星,航向精度评估函数再以几何强度与信号品质遴选最优子集。该分层流程显著增强系统对环境变化的鲁棒性,提升航向精度与稳定性,降低计算负载,使系统在复杂环境下始终稳健、连续且高精度地给出航向。
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