2019
DOI: 10.1049/iet-cta.2018.5477
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Finite‐time disturbance observer based integral sliding mode control for attitude stabilisation under actuator failure

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Cited by 57 publications
(45 citation statements)
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“…Substituting the proposed PD position controller (11) with (16) into (13) results in a closed-loop error system:…”
Section: Part One: Global Asymptotic Stabilitymentioning
confidence: 99%
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“…Substituting the proposed PD position controller (11) with (16) into (13) results in a closed-loop error system:…”
Section: Part One: Global Asymptotic Stabilitymentioning
confidence: 99%
“…This kind of method has poor adaptability for different constraints, and some tracking performance is sacrificed. In recent years, some high-performance control strategies have been proposed for dynamic and steady-state performance of several kinds of state constrained systems [12][13][14][15][16][17][18][19] and for spacecraft systems. [20][21][22][23][24][25][26][27] This article focuses on designing a method of constraint control to solve the position tracking control problem for quad-rotor system with velocity constrains.…”
Section: Introductionmentioning
confidence: 99%
“…Multimodel adaptive control methods were employed as a fault compensation in literatures [6][7][8]. Literatures [9][10][11] applied neural network to the design of reconfigurable aircraft control in the case of sensors or actuator faults. The fault recognition and faulttolerant control strategies of the near space vehicle are designed base on the adaptive sliding mode control method in reference [12].…”
Section: Introductionmentioning
confidence: 99%
“…The disturbance observer, which is famous due to its precise estimation for disturbances, has also been widely researched in aerospace engineering [20]- [25]. In [20], the robustness of the spacecraft attitude control system is significantly enhanced by resorting to a specially designed disturbance observer, which can effectively estimate the external disturbance.…”
Section: Introductionmentioning
confidence: 99%
“…As a further technological extension, two disturbance observers have been established in [17] and [21] such that the formation task could be accomplished under seriously disturbed environment. Considering for the convergence rate, controllers proposed in [21]- [25] possess finite-time stability. Especially, methods in [23] is capable of tackling the actuator fault and the input saturation constraint will not be violated in [24], [25].…”
Section: Introductionmentioning
confidence: 99%