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Unknown input recovery for closed loop systems with saturations

机译:饱和的闭环系统的未知输入恢复

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An inverse method is developed to recover for unknown stochastic inputs. The proposed approach relies on an approximate finite impulse response model of the system which is seen as a linearization around the current input estimation. The inversion itself is done within the frequency domain in order to lower the computation cost. This classical approach requires a regularization technique to be used in order to limit sensitivity to noise. Several tools are discussed here, including shaping filters. An original procedure is then introduced for the automatic tuning of the regularization parameters. It is justified by a SVD analysis. The second main contribution is the saturation effects processing. These effects are taken into account for by separating inversion of the linear and nonlinear parts of the output error. This original method relies on the projection of signals on a dedicated basis. The overall procedure is applied to the recovery of the roll rate of an aircraft that is induced by a spatially non uniform turbulent wind along the wing. Such an input is not measured. Its estimation allows to minimize the difference between the recorder lateral displacement of the plane with respect to the runway axis and the simulated one.
机译:开发了一种逆方法来恢复未知的随机输入。所提出的方法依赖于系统的近似有限脉冲响应模型,该模型被视为围绕当前输入估计的线性化。为了降低计算成本,反演本身在频域内完成。这种经典方法要求使用正则化技术以限制对噪声的敏感性。这里讨论了几种工具,包括整形过滤器。然后引入原始过程以自动调整正则化参数。通过SVD分析可以证明这一点。第二个主要贡献是饱和效果处理。通过分离输出误差的线性和非线性部分的反转来考虑这些影响。这种原始方法依赖于专用的信号投影。整个过程适用于飞机机翼侧倾率的恢复,这是由沿机翼的空间上不均匀的湍流风引起的。此类输入未测量。它的估计可以使飞机相对于跑道轴线的记录仪横向位移与模拟的轴向位移之间的差异最小。

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