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Fractional-order complementary filters for small unmanned aerial system attitude estimation

机译:分数阶互补滤波器,用于小型无人航空系统姿态估计

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For small unmanned aerial systems (sUAS), the problem of estimation of orientation angles relative to the Earths surface (attitude) is of major importance. Usually, this estimation is performed by the combination of several kinds of sensor data by a Kalman filter or complementary-style filter producing a navigation-quality solution. Kalman filters make assumptions about linearity and statistical properties of the sensor noise, which must be accurate for proper functioning of the filter. Another option, the complementary filter, is more simple, and does not make these assumptions. Although the applications of the complementary filter have been researched in depth, the complementary filter can be combined in a novel way with fractional-order filters for the purpose of small UAS flight. In this paper, a roll-pitch fractional-order estimator is shown in flight configuration (real-time code) on a small sUAS. With fewer tunable parameters, we show that the fractional-order filter is more simple to implement. Realtime results are shown which indicate adequate performance relative to an existing quaternion-based Kalman filter-based estimator.
机译:对于小型无人机系统(sUAS),相对于地球表面(姿态)的方位角估计问题非常重要。通常,这种估计是通过卡尔曼滤波器或互补型滤波器对几种传感器数据进行组合来产生导航质量解决方案来执行的。卡尔曼滤波器对传感器噪声的线性和统计特性做出假设,这些假设对于滤波器的正常运行必须是准确的。另一个选择是互补滤波器,它更简单,并且不作这些假设。尽管已经对互补滤波器的应用进行了深入研究,但是出于小型UAS飞行的目的,可以以新颖的方式将互补滤波器与分数阶滤波器组合。在本文中,在小型sUAS上的飞行配置(实时代码)中显示了滚动俯仰分数阶估计器。用更少的可调参数,我们表明分数阶滤波器更易于实现。示出了实时结果,其指示相对于现有的基于四元数的基于卡尔曼滤波器的估计器而言足够的性能。

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