2018
DOI: 10.1109/tie.2017.2772153
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An Adaptive Fault-Tolerant Sliding Mode Control Allocation Scheme for Multirotor Helicopter Subject to Simultaneous Actuator Faults

Abstract: This paper proposes a novel adaptive sliding mode based control allocation scheme for accommodating simultaneous actuator faults. The proposed control scheme includes two separate control modules with virtual control part and control allocation part, respectively. As a lowlevel control module, the control allocation/re-allocation scheme is used to distribute/redistribute virtual control signals among the available actuators under fault-free or faulty cases, respectively. In the case of simultaneous actuator fa… Show more

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Cited by 140 publications
(59 citation statements)
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“…The sliding-mode control has been used extensively to deal with fault-tolerant control (see, e.g. [21]- [22], [25]- [27]). However, the uncertainty existing in the input distribution matrix are rarely considered in the existing work, and specifically, the associate result for high-speed train has not been available.…”
Section: Remarkmentioning
confidence: 99%
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“…The sliding-mode control has been used extensively to deal with fault-tolerant control (see, e.g. [21]- [22], [25]- [27]). However, the uncertainty existing in the input distribution matrix are rarely considered in the existing work, and specifically, the associate result for high-speed train has not been available.…”
Section: Remarkmentioning
confidence: 99%
“…There are many results about the fault-tolerant sliding-mode control design (see for example [21]- [22], [25]- [27]). However, the considered faults are always assumed to have known bounds or more information of faults, except the contributions mentioned in Remark 4.…”
Section: Remarkmentioning
confidence: 99%
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“…Fault‐tolerant flight control (FTC) schemes have been studied extensively in the literature . The dynamic model of an aircraft changes significantly after the fault occurrence, which leads to reduced effectiveness of the controllers that are designed based on a nominal model and in some cases the closed‐loop system becomes unstable after the fault occurrence.…”
Section: Introductionmentioning
confidence: 99%
“…It is easy to implement and can deal with nonlinear part of dynamic systems, satisfactorily. In addition, due to the robustness of the SMC, it can be used satisfactorily to maintain the closed-loop performance in the presence of model uncertainties and external disturbances [2].…”
Section: Introductionmentioning
confidence: 99%