Robust visual pose measurement and uncertainty suppression for UAVs in dynamic landing environments

计算机科学 控制理论(社会学) 卡尔曼滤波器 不确定性传播 滤波器(信号处理) 离群值 人工智能 测量不确定度 可观测性 传感器融合 协方差 水准点(测量) 灵敏度(控制系统) 鲁棒控制 计算机视觉 特征(语言学) 联轴节(管道) 均方误差 区间(图论) 扩展卡尔曼滤波器 模拟 蒙特卡罗方法 边界(拓扑) 保险丝(电气) 协方差矩阵 融合机制 观测误差 算法 计量系统 噪音(视频) 比例因子(宇宙学) 计量学 架空(工程) 融合
作者
Pingping Qu,Yeshan Chen,Tengli Yu,Jing Guo,Yubin Xu,Song Xu,Ershen wang,Feng Wang,Changlong Chen
出处
期刊:Measurement Science and Technology [IOP Publishing]
卷期号:37 (12): 126304-126304 被引量:1
标识
DOI:10.1088/1361-6501/ae532f
摘要

Abstract High-precision relative attitude measurement is a critical prerequisite for autonomous recovery of micro unmanned aerial vehicles (UAVs) in GNSS-restricted and dynamic environments. However, motion blur and drastic scale changes often lead to a surge in visual observation noise, causing significant drift in state estimation. To address this, this paper proposes a holistic visual metrology system that deeply fuses enhanced perception with uncertainty suppression. First, at the perception layer, an improved YOLO11n-Landing network serves as a high-fidelity instrument, utilizing multi-scale feature enhancement and anti-blur attention mechanisms to boost detection confidence in dynamic scenes. Second, a height-constrained Kalman filter was constructed at the fusion layer, explicitly managing uncertainty propagation through a physical covariance model. The validity of the optimal fusion interval was confirmed based on parameter sensitivity analysis. Crucially, at the system level, a perception-control coupled isolation mechanism has been introduced. Unlike traditional loosely coupled architectures, this mechanism uses the visual confidence factor as an information hub, synchronously mapping it to the filter covariance, switching gain K , and boundary layer thickness. This dynamically reconstructs the system’s response bandwidth, actively isolating invalid observations, and physically blocking the propagation of measurement outliers into the control loop. Experimental results demonstrate that compared to traditional benchmark methods, this integrated system significantly converges the root mean square error to 0.156 m, reduces the error variance by approximately 74.7%, and achieves a 99.0% landing success rate in Monte Carlo simulations. This work not only provides a highly system-integrity-preserving technical solution for robust autonomous landing of micro UAVs, but its core coupling paradigm also demonstrates broad prospects for generalization to high-risk tasks such as aerial docking and close-range inspection.

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