跑道
全球定位系统
惯性导航系统
计算机科学
卡尔曼滤波器
计算机视觉
惯性测量装置
人工智能
弹道
方向(向量空间)
电信
考古
物理
历史
天文
数学
几何学
作者
Lei Zhang,Zhengjun Zhai,Lang He,Wensheng Niu
出处
期刊:IEEE Access
[Institute of Electrical and Electronics Engineers]
日期:2019-01-01
卷期号:7: 28684-28695
被引量:17
标识
DOI:10.1109/access.2019.2893062
摘要
Precise navigation is a fundamental problem of aircraft safety approach and landing. However, the existing methods, including rotorcraft-based and fixed-wing-based, cannot meet the requirements of precision approach and landing of civil aircraft in the global position system (GPS)-denied and low visibility. This paper proposes an autonomous approach and landing navigation method whose accuracy is comparable to Inertial/Differential GPS (DGPS) integration. This method integrates inertial data, forward-looking infrared (FLIR) images, and runway geographic information to estimate kinetics states of aircraft during approach and landing. First, we improve an existing method to robustly detect runway, accurately extract three vertexes of runway contour from FLIR images, and synthesize the virtual runway features by runway geo-information and aircraft's pose parameters. Second, we propose to use real and synthetic runway features to create vision cues and integrate them with inertial data in square-root unscented Kalman filter to estimate the motion errors. Meanwhile, the measured motion states are corrected with the estimated state errors. Finally, we design a flight data acquisition platform equipped on a general aircraft and use the real flight data to verify our proposed method. The experimental results demonstrate that the proposed method can run smoothly for civil aircraft precision approach and landing.
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