Novel Direct and Accurate Identification of Kalman Filter for General Systems Described by a Box-Jenkins Model

R. Doraiswami, L. Cheded
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引用次数: 3

Abstract

A novel robust Kalman filter (KF)-based controller is proposed for a multivari-able system to accurately track a specified trajectory under unknown stochastic disturbance and measurement noise. The output is a sum of uncorrelated signal, disturbance and measurement noise. The system model is observable but not controllable while the signal one is controllable and observable. An emulator-based two-stage identification is employed to obtain a robust model needed to design the robust controller. The system and KF are identified and the signal and output error estimated. From the identified models, minimal realizations of the signal and KF, the disturbance model and whitening filter are obtained using balanced model reduction techniques. It is shown that the signal model is a transfer matrix relating the system output and the KF residual, and the residual is the whitened output error. The disturbance model is identified by inverse filtering. A feedback-feedforward controller is designed and implemented using an internal model of the reference driven by the error between the reference and the signal estimate, the feedforward of reference and output error. The successful evaluation of the proposed scheme on a simulated autonomously-guided drone gives ample encouragement to test it later, on a real one.
基于Box-Jenkins模型的通用系统卡尔曼滤波直接准确辨识方法
针对多变量系统在未知随机干扰和测量噪声下精确跟踪指定轨迹的问题,提出了一种基于鲁棒卡尔曼滤波(KF)的控制器。输出是不相关信号、干扰和测量噪声的总和。系统模型是可观察的但不可控制的,而信号模型是可控制的和可观察的。采用基于仿真器的两阶段辨识方法,得到设计鲁棒控制器所需的鲁棒模型。对系统和KF进行辨识,并对信号和输出误差进行估计。从识别的模型中,利用平衡模型约简技术得到信号和KF的最小实现、干扰模型和白化滤波器。结果表明,信号模型是系统输出与KF残差之间的传递矩阵,残差是输出误差的白化。采用反滤波方法对扰动模型进行辨识。利用参考点与信号估计值之间的误差、参考点的前馈和输出误差驱动的参考点内部模型,设计并实现了反馈-前馈控制器。该方案在一架模拟自主制导无人机上的成功评估,给了我们足够的鼓励,让我们以后在一架真正的无人机上进行测试。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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