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Flexible Stereo: Constrained, Non-Rigid, Wide-Baseline Stereo Vision for Fixed-Wing Aerial Platforms

机译:灵活的立体声:限制,非刚性,宽基线立体声立体声视野,用于固定翼空中平台

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This paper proposes a computationally efficient method to estimate the time-varying relative pose between two visual-inertial sensor rigs mounted on the flexible wings of a fixed-wing unmanned aerial vehicle (UAV). The estimated relative poses are used to generate highly accurate depth maps in real-time and can be employed for obstacle avoidance in low-altitude flights or landing maneuvers. The approach is structured as follows: Initially, a wing model is identified by fitting a probability density function to measured deviations from the nominal relative baseline transformation. At run-time, the prior knowledge about the wing model is fused in an Extended Kalman filter (EKF) together with relative pose measurements obtained from solving a relative perspective N-point problem (PNP), and the linear accelerations and angular velocities measured by the two inertial measurement units (IMU) which are rigidly attached to the cameras. Results obtained from extensive synthetic experiments demonstrate that our proposed framework is able to estimate highly accurate baseline transformations and depth maps.
机译:本文提出了一种计算上有效的方法来估计安装在固定翼无人驾驶车辆(UAV)的柔性翼上安装在柔性翼的两个视觉惯性传感器钻机之间的时变相对姿势。估计的相对姿势用于实时产生高度精确的深度图,可以用于低空飞行或降落操纵中的避免障碍物。该方法如下结构:首先,通过拟合概率密度函数来识别翼型模型,以从标称相对基线变换测量偏差。在运行时,关于机翼模型的先前知识在扩展卡尔曼滤波器(EKF)中融合,以及从求解相对透视n点问题(PNP)的相对姿势测量,以及测量的线性加速度和角速度刚性地附接到相机的两个惯性测量单元(IMU)。从广泛的合成实验获得的结果表明我们所提出的框架能够估计高度准确的基线变换和深度图。

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