航空学报 > 2026, Vol. 47 Issue (7): 332837-332837   doi: 10.7527/S1000-6893.2025.32837

一种基于线性约束的鲁棒几何滤波方法

金宇强, 杨旭升, 张文安()   

  1. 浙江工业大学 信息工程学院,杭州 310014
  • 收稿日期:2025-09-28 修回日期:2025-10-24 接受日期:2025-11-18 出版日期:2025-12-01 发布日期:2025-11-28
  • 通讯作者: 张文安
  • 基金资助:
    国家自然科学基金重点(联合)项目(U25A20456); 杭州市重大科技创新项目(2022AIZD0080)

Robust geometric filtering via linear constraint

Yuqiang JIN, Xusheng YANG, Wenan ZHANG()   

  1. College of Information Engineering,Zhejiang University of Technology,Hangzhou 310014,China
  • Received:2025-09-28 Revised:2025-10-24 Accepted:2025-11-18 Online:2025-12-01 Published:2025-11-28
  • Contact: Wenan ZHANG
  • Supported by:
    National Natural Science Foundation of China(U25A20456); Major Science and Technology Innovation Project of Hangzhou(2022AIZD0080)

摘要:

针对几何滤波结果对模型失配敏感的问题,提出了一种线性约束方法。首先,通过分析群仿射系统中模型失配对滤波过程的影响机制,揭示了标准几何滤波(如不变扩展卡尔曼滤波(InEKF))在模型失配时误差累积的本质原因。其次,设计了一种线性约束滤波方法,通过约束滤波增益矩阵在模型偏差方向上的行为来抑制误差传播,同时保持李群流形上的几何特性。该方法在保持实时性的情况下,有效提升了系统对模型失配的鲁棒性。最后,通过惯性导航与全球卫星导航系统(INS/GNSS)组合导航的仿真与实验表明:所提方法相较标准不变扩展卡尔曼滤波的估计精度上均取得显著提升,为复杂环境下的鲁棒滤波提供了有效解决方案。

关键词: 几何滤波, 模型失配, 鲁棒估计, 卡尔曼滤波, 李群与李代数

Abstract:

To address the sensitivity of geometric filtering results to model mismatch, this paper introduces a novel filtering framework grounded in linear constraint enforcement. We begin by analyzing how model mismatch propagates through the filtering process in group-affine systems, revealing the fundamental mechanism behind model mismatch accumulation in conventional geometric filters such as the Invariant Extended Kalman Filter (InEKF). Second, we design a constrained filtering strategy that actively regulates the gain matrix along the direction of model deviation, thereby suppressing model mismatch growth while preserving the intrinsic geometric structure of the underlying Lie group manifold. Notably, the proposed method achieves this enhanced robustness without sacrificing computational efficiency, making it suitable for real-time deployment. Finally, simulations and real-world experiments on INS/GNSS (Inertial Navigation System/Global Navigation Satellite System) integrated navigation demonstrate that the proposed method consistently achieves substantially improved estimation accuracy compared to the standard InEKF, offering an effective solution for robust filtering in complex environments.

Key words: geometric filtering, model mismatch, robust estimation, Kalman filter, Lie groups and Lie algebras

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