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A REAL-TIME MODEL ERROR FILTER AND STATE ESTIMATOR

机译:实时模型错误过滤器和状态估计器

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摘要

In this paper, a new real-time filter and state estimator is developed which provides a method of determining optimal state estimates in the presence of significant error in the assumed (nominal) model. Also, the new algorithm is able to determine actual model-error time histories using sequential measurements. The real-time filter/state estimator is derived for continuous systems. The functional form for this case involves the determination of an algebraic Riccati equation, a Lyapunov equation, and a linear equation to determine the gain matrix used in the filter design. Three examples are shown which demonstrate the usefulness of this new algorithm. The first example involves the estimation of a single state using no assumed model. The second example involves the estimation of the nonlinear trajectory of Van der Pol's equation using a linear state model matrix. The third example involves the estimation of the orientation of a highly maneuverable fighter aircraft using an inaccurate system model. Results indicate that this new algorithm is able to determine accurate state estimates in the presence of significant errors in the assumed model.
机译:在本文中,开发了一种新的实时滤波器和状态估计器,它提供了一种在假定(标称)模型中存在重大误差的情况下确定最佳状态估计的方法。而且,新算法能够使用顺序测量来确定实际的模型误差时间历史记录。实时滤波器/状态估计器适用于连续系统。这种情况的函数形式包括确定代数Riccati方程,Lyapunov方程和线性方程,以确定滤波器设计中使用的增益矩阵。显示了三个示例,这些示例演示了此新算法的有用性。第一个示例涉及不使用假定模型的单个状态的估计。第二个示例涉及使用线性状态模型矩阵估算Van der Pol方程的非线性轨迹。第三个示例涉及使用不准确的系统模型估算高度机动的战斗机的方向。结果表明,该新算法能够在假定模型中存在重大错误的情况下确定准确的状态估计。

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