2019
DOI: 10.1016/j.isatra.2019.02.028
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Disturbance suppression for quadrotor UAV using sliding-mode-observer-based equivalent-input-disturbance approach

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Cited by 70 publications
(29 citation statements)
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“…Since the right-hand side of the Equation 1has discontinuous terms, their solutions are understood in the Filippov sense (see [7]). It is assumed that the full vector state of the dynamic system (1) is available for measurement; note that this assumption is not restrictive because there are several works in the literature about observers and differentiators design (see [4], [5], [6], [10], [14], and references quoted therein).…”
Section: A Considered Systemsmentioning
confidence: 99%
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“…Since the right-hand side of the Equation 1has discontinuous terms, their solutions are understood in the Filippov sense (see [7]). It is assumed that the full vector state of the dynamic system (1) is available for measurement; note that this assumption is not restrictive because there are several works in the literature about observers and differentiators design (see [4], [5], [6], [10], [14], and references quoted therein).…”
Section: A Considered Systemsmentioning
confidence: 99%
“…In this work, numerical results of a generalization of the set of control laws in [13] are obtained using a one-link pendulum as a testbed. A PD control law is added to the set of controllers (6) in order to compensate external disturbances described by Equation (4). A sketch of the main results of this paper will be developed in the following sections.…”
Section: B Mathematical Backgroundmentioning
confidence: 99%
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“…Many studies of extended sliding mode control have been published to overcome the effects of chattering phenomenon, parameter uncertainties, and external disturbances. In [21,22], sliding mode control with disturbance observer was proposed for rejecting the effect of the unknown disturbance in the quadrotor while achieving the performance of attitude control and disturbance suppression. In [23,24] backstepping sliding mode control technique was presented to accomplish quadrotor altitude, attitude and trajectory tracking control performance.…”
Section: Introductionmentioning
confidence: 99%
“…(1) Compared with the neural networks (NN)-based observers [30]- [33], [50], [51] and the nonlinear ESO [59]- [62] requiring the multiple states information and complex nonlinear coefficients, the LESO employed in the control scheme is intuitively designed based on the state feedback, and the tuning operation is rather simple since linear observer parameters are utilized. (2) Rather than the nonlinear disturbances observers [45]- [49], [64]- [67] and other ESO [59]- [63] based on the position feedback, the 2 nd -order LESO with velocity feedback is developed. In practice, the velocity information is easily acquired, which is more accurate and reliable, especially for the multi-rotor UAVs.…”
Section: Introductionmentioning
confidence: 99%