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Multirate and event-driven Kalman filters for helicopter flight

机译:用于直升机飞行的多速率和事件驱动的卡尔曼滤波器

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摘要

A vision-based obstacle detection system that provides information about objects as a function of azimuth and elevation is discussed. The range map is computed using a sequence of images from a passive sensor, and an extended Kalman filter is used to estimate range to obstacles. The magnitude of the optical flow that provides measurements for each Kalman filter varies significantly over the image depending on the helicopter motion and object location. In a standard Kalman filter, the measurement update takes place at fixed intervals. It may be necessary to use a different measurement update rate in different parts of the image in order to maintain the same signal to noise ratio in the optical flow calculations. A range estimation scheme that accepts the measurement only under certain conditions is presented. The estimation results from the standard Kalman filter are compared with results from a multirate Kalman filter and an event-driven Kalman filter for a sequence of helicopter flight images.
机译:讨论了基于视觉的障碍物检测系统,该系统根据方位角和仰角提供有关对象的信息。使用来自无源传感器的一系列图像来计算距离图,并且使用扩展的卡尔曼滤波器来估计到障碍物的距离。根据直升机的运动和物体的位置,为每个卡尔曼滤波器提供测量值的光流大小在整个图像上会有很大变化。在标准卡尔曼滤波器中,测量更新以固定间隔进行。为了在光流计算中保持相同的信噪比,可能有必要在图像的不同部分使用不同的测量更新率。提出了仅在特定条件下接受测量的范围估计方案。将标准卡尔曼滤波器的估计结果与多速率卡尔曼滤波器和事件驱动的卡尔曼滤波器的结果进行比较,以获取一系列直升机飞行图像。

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