52nd IEEE Conference on Decision and Control 2013
DOI: 10.1109/cdc.2013.6760755
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Dynamic state estimation in distributed aircraft electric control systems via adaptive submodularity

Abstract: Abstract-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 stra… Show more

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Cited by 8 publications
(8 citation statements)
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“…PERSISTENT SENSOR FAULTS We are motivated by the discrete state estimation problem of an aircraft electrical system via active sensing, first studied in [10] (see Figure 1 for an example of a simple circuit and the readers are referred to [10] for a detailed description of the electrical circuits). As more systems become more dependent on electric power systems, this problem is crucial to the safety of these systems.…”
Section: Motivation: Aircraft Electrical System Withmentioning
confidence: 99%
See 2 more Smart Citations
“…PERSISTENT SENSOR FAULTS We are motivated by the discrete state estimation problem of an aircraft electrical system via active sensing, first studied in [10] (see Figure 1 for an example of a simple circuit and the readers are referred to [10] for a detailed description of the electrical circuits). As more systems become more dependent on electric power systems, this problem is crucial to the safety of these systems.…”
Section: Motivation: Aircraft Electrical System Withmentioning
confidence: 99%
“…Despite persistent faults, our goal is similar to that in [10], i.e., to design a policy that can adaptively estimate the discrete state of the circuit by taking "actions" (i.e., opening or closing controllable contactors) and observing the sensor measurements. Note that we are only interested in estimating the unknown discrete state of the system and not the true failure mode of the sensors.…”
Section: Motivation: Aircraft Electrical System Withmentioning
confidence: 99%
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“…As summarized in Section I, several algorithms have been proposed for minimizing or maximizing a submodular function. Its application includes sensor placement [39], [40], actuator placement (based on the controllability Grammian) [41], network inference [42], dynamic state estimation [43], and leader selection under link noise [44].…”
Section: Comparison With Submodularitymentioning
confidence: 99%
“…For aircraft electric power systems, switching contactors can be used to route power as needs change or faults occur. There are numerous questions that can be formulated in this setting, such as switching to identify faults when there are limited sensors available [8].…”
Section: Example: Aircraft Electric Power Systemmentioning
confidence: 99%