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The Enriched Sigma Point Kalman Filter: An adaptation of the Unscented Kalman Filter for Navigation Applications

机译:丰富的Sigma Point Kalman滤波器:适应Unscented Kalman滤波器的导航应用程序

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The Unscented Kalman Filter (UKF) has received a lot of attention in the last few years, especially for inertial navigation applications. Indeed, it efficiently extends the nonlinear capacities of the Extended Kalman Filter (EKF), and provides additional benefits, such as an absence of divergence and a black-box implementation that simplifies the maintenance of such an algorithm. Nevertheless, during the heading determination phase of an inertial navigation algorithm, the barycentre of the unscented transform used to represent the system state is not adapted because it creates an artificial position error. An alternative algorithm, using a so-called 'Central point' allows to benefit from the UKF capabilities while suppressing this drawback, making it possible to determine the heading of a system without any of the static constraints of a traditional inertial navigation system.
机译:在过去几年中,Unscented Kalman滤波器(UKF)在惯性导航应用中受到了很多关注。实际上,它有效地扩展了扩展卡尔曼滤波器(EKF)的非线性容量,并提供了额外的益处,例如没有发散和黑盒实现,简化了这种算法的维护。然而,在惯性导航算法的标题确定阶段期间,用于表示系统状态的Unscented变换的重构不适应,因为它创造了人工位置误差。使用所谓的“中心点”的替代算法允许从UKF功能中受益,同时抑制该缺点,使得可以确定没有传统惯性导航系统的任何静态约束的系统的标题。

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