Fault Detection and Isolation for a 3-DOF Helicopter with Sliding Mode Strategies

U. Perez, E. Capello, Elisabetta Punta, J. Perea, L. Fridman
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引用次数: 4

Abstract

This paper analyzes the problem of detection and isolation of faults in the actuators of a 3-Degree-of-Freedom (3-DOF) helicopter by a residual-based approach. A third-order sliding mode differentiator is designed for the evaluation of the residuals. Moreover, two sliding mode controllers are suitably designed to stabilize the angular positions and velocities: (i) a super twisting control system and (ii) a continuous twisting control system. The performance of the designed controllers and the effectiveness of the residual-based method are illustrated by simulations.
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基于滑模策略的三自由度直升机故障检测与隔离
本文用残差法分析了三自由度直升机执行机构故障的检测与隔离问题。设计了一个三阶滑模微分器用于残差的估计。此外,还设计了两个滑模控制器来稳定角位置和角速度:(i)超扭控制系统和(ii)连续扭控制系统。仿真结果验证了所设计控制器的性能和基于残差的方法的有效性。
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