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Dynamic state estimation in distributed aircraft electric control systems via adaptive submodularity

机译:基于自适应亚模量的分布式飞机电控系统动态状态估计

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We consider the problem of estimating the discrete state of an aircraft electric system under a distributed control architecture through active sensing. The main idea is to use a set of controllable switches to reconfigure the system in order to gather more information about the unknown state. By adaptively making a sequence of reconfiguration decisions with uncertain outcome, then correlating measurements and prior information to make the next decision, we aim to reduce the uncertainty. A greedy strategy is developed that maximizes the one-step expected uncertainty reduction. By exploiting recent results on adaptive submodularity, we give theoretical guarantees on the worst-case performance of the greedy strategy. We apply the proposed method in a fault detection scenario where the discrete state captures possible faults in various circuit components. In addition, simple abstraction rules are proposed to alleviate state space explosion and to scale up the strategy. Finally, the efficiency of the proposed method is demonstrated empirically on different circuits.
机译:我们考虑了通过主动感应来估计分布式控制架构下飞机电气系统离散状态的问题。主要思想是使用一组可控开关来重新配置系统,以便收集有关未知状态的更多信息。通过自适应地做出具有不确定结果的一系列重配置决策,然后将测量值和先前的信息相关联以做出下一个决策,我们旨在减少不确定性。制定了一种贪婪策略,可最大程度地减少预期的单步不确定性。通过利用有关自适应亚模态的最新结果,我们为贪婪策略的最坏情况下的性能提供了理论上的保证。我们将提出的方法应用于故障检测场景中,其中离散状态捕获了各种电路组件中的可能故障。另外,提出了简单的抽象规则来减轻状态空间爆炸并扩大策略。最后,在不同电路上通过经验证明了所提方法的效率。

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