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Infrared-Inertial Navigation for Commercial Aircraft Precision Landing in Low Visibility and GPS-Denied Environments

机译:低能见度和GPS拒绝环境下的商用飞机精确着陆的红外惯性导航

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摘要

This paper proposes a novel infrared-inertial navigation method for the precise landing of commercial aircraft in low visibility and Global Position System (GPS)-denied environments. Within a Square-root Unscented Kalman Filter (SR_UKF), inertial measurement unit (IMU) data, forward-looking infrared (FLIR) images and airport geo-information are integrated to estimate the position, velocity and attitude of the aircraft during landing. Homography between the synthetic image and the real image which implicates the camera pose deviations is created as vision measurement. To accurately extract real runway features, the current results of runway detection are used as the prior knowledge for the next frame detection. To avoid possible homography decomposition solutions, it is directly converted to a vector and fed to the SR_UKF. Moreover, the proposed navigation system is proven to be observable by nonlinear observability analysis. Last but not least, a general aircraft was elaborately equipped with vision and inertial sensors to collect flight data for algorithm verification. The experimental results have demonstrated that the proposed method could be used for the precise landing of commercial aircraft in low visibility and GPS-denied environments.
机译:本文提出了一种新颖的红外惯性导航方法,用于在低能见度和全球定位系统(GPS)受限的环境中精确地商用飞机降落。在平方根无味卡尔曼滤波器(SR_UKF)中,惯性测量单位(IMU)数据,前视红外(FLIR)图像和机场地理信息被集成在一起,以估计飞机着陆期间的位置,速度和姿态。合成图像和真实图像之间的同相照相法包含了相机的姿势偏差,并以此作为视觉测量。为了准确地提取真实的跑道特征,将跑道检测的当前结果用作下一帧检测的先验知识。为避免可能的单应性分解解决方案,将其直接转换为向量,然后馈入SR_UKF。此外,通过非线性可观察性分析证明了所提出的导航系统是可观察的。最后但并非最不重要的一点是,一架通用飞机精心配备了视觉和惯性传感器,以收集飞行数据以进行算法验证。实验结果表明,该方法可用于低能见度和GPS拒绝环境下的商用飞机精确着陆。

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