2015
DOI: 10.1002/acs.2585
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Adaptive compensation for infinite number of actuator failures with an application to flight control

Abstract: SummaryIn this paper, a new adaptive compensation control scheme is proposed for a class of nonlinear systems with unknown parameters and unknown actuator failures. The normal operation case and different failure cases of actuators are unified through a time‐varying model. By introducing a smooth function, an integrable auxiliary signal, and a bound estimation approach, the effect of failures is successfully compensated for, and the total number of failures is not restricted to be finite. It is shown that all … Show more

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Cited by 15 publications
(2 citation statements)
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References 23 publications
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“…It is convenient for the internal dynamics of the actuator is ignored. In this paper, similar to [47, 48], actuators operate in a fault model, and it can be modelled as right left right left right left right left right left right left0.278em 2em 0.278em 2em 0.278em 2em 0.278em 2em 0.278em 2em 0.278em3ptuj=wj,rvj+ufalse¯j,r,thinmathspacet[Gj,ra,Gj,rb),wj,rufalse¯j,r=0,r=1,2,3,thinmathspacewhere uj is the output of the j th actuator, vj is the event‐triggered input and the input of the j th actuator, 0<wj,r1 and u¯j,r is the unknown constant representing different actuator fault models, Gj,ra is the time at j th actuator fault begins and Gj,rb is the time at the j th actuator fault ends.…”
Section: Problem Formulation and Preliminariesmentioning
confidence: 90%
“…It is convenient for the internal dynamics of the actuator is ignored. In this paper, similar to [47, 48], actuators operate in a fault model, and it can be modelled as right left right left right left right left right left right left0.278em 2em 0.278em 2em 0.278em 2em 0.278em 2em 0.278em 2em 0.278em3ptuj=wj,rvj+ufalse¯j,r,thinmathspacet[Gj,ra,Gj,rb),wj,rufalse¯j,r=0,r=1,2,3,thinmathspacewhere uj is the output of the j th actuator, vj is the event‐triggered input and the input of the j th actuator, 0<wj,r1 and u¯j,r is the unknown constant representing different actuator fault models, Gj,ra is the time at j th actuator fault begins and Gj,rb is the time at the j th actuator fault ends.…”
Section: Problem Formulation and Preliminariesmentioning
confidence: 90%
“…Taking into account the importance of this feature for a controller, in Xing et al (2017b) the control method of Xing et al (2017a) has been strengthened to deal with actuator failures. In Xing et al (2017b), an adaptive event-triggered approach for control of a class of nonlinear systems with parametric uncertainty and fault in actuators has been proposed by considering the actuator failures modelled in Wang and Guo (2015) and Wang and Wen (2010). It is worth noting that the control method introduced in Xing et al (2017a), similar to that presented in Xing et al (2017b), does not cover the case that the direction of control is unknown because the information of the sign of the function specifying the input direction is used in obtaining the control efforts in these methods.…”
Section: Introductionmentioning
confidence: 99%