首页> 外文期刊>International Journal of Applied Mathematics and Computer Science >ROBUST MULTIPLE SENSOR FAULT-TOLERANT CONTROL FOR DYNAMIC NON-LINEAR SYSTEMS: APPLICATION TO THE AERODYNAMICAL TWIN-ROTOR SYSTEM
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ROBUST MULTIPLE SENSOR FAULT-TOLERANT CONTROL FOR DYNAMIC NON-LINEAR SYSTEMS: APPLICATION TO THE AERODYNAMICAL TWIN-ROTOR SYSTEM

机译:动态非线性系统的鲁棒多传感器容错控制:在航空双转子系统中的应用

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摘要

The paper deals with the problem of designing sensor-fault tolerant control for a class of non-linear systems. The scheme is composed of a robust state and fault estimator as well as a controller. The estimator aims at recovering the real system state irrespective of sensor faults. Subsequently, the fault-free state is used for control purposes. Also, the robust sensor fault estimator is developed in a such a way that a level of disturbances attenuation can be reached pertaining to the fault estimation error. Fault-tolerant control is designed using similar criteria. Moreover, a separation principle is proposed, which makes it possible to design the fault estimator and control separately. The final part of the paper is devoted to the comprehensive experimental study related to the application of the proposed approach to a non-linear twin-rotor system, which clearly exhibits the performance of the new strategy.
机译:本文针对一类非线性系统设计传感器容错控制问题。该方案由鲁棒状态和故障估计器以及控制器组成。估计器旨在恢复实际系统状态,而与传感器故障无关。随后,将无故障状态用于控制目的。同样,以这样的方式开发鲁棒的传感器故障估计器,使得可以达到与故障估计误差有关的干扰衰减水平。容错控制使用相似的标准进行设计。此外,提出了分离原理,这使得可以分开设计故障估计器和控制。本文的最后一部分致力于与所提出的方法在非线性双转子系统中的应用有关的综合实验研究,清楚地展示了该新策略的性能。

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