2020
DOI: 10.1007/s11424-020-9306-6
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A Second-Order Sliding Mode Controller of Quad-Rotor UAV Based on PID Sliding Mode Surface with Unbalanced Load

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Cited by 27 publications
(12 citation statements)
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“…This work uses a fully controlled four-engine model similar to that of [14]. The simulated model is based on the dynamic equations used in [14], [15], and [16]. The model is divided into body rotation dynamics, through the angles ϕ (roll angle), θ (pitch angle), and ψ (yaw angle), and translation in Cartesian axes, as show in Fig.…”
Section: Quadcopter Modelingmentioning
confidence: 99%
“…This work uses a fully controlled four-engine model similar to that of [14]. The simulated model is based on the dynamic equations used in [14], [15], and [16]. The model is divided into body rotation dynamics, through the angles ϕ (roll angle), θ (pitch angle), and ψ (yaw angle), and translation in Cartesian axes, as show in Fig.…”
Section: Quadcopter Modelingmentioning
confidence: 99%
“…To highlight the unmanned concept in CAAC, we manage to apply a second-order sliding mode flight controller (SFC) to the given six-DOF flight model [18]. The logic is to ensure that the system states can converge to the sliding mode manifolds = = 0 in limited time with reference to appropriate control laws [19]- [21]. Rewrite (1) into the following form:…”
Section: Tablementioning
confidence: 99%
“…In order to improve control efficiency, PID control [8], backstepping control [9], sliding mode control (SMC) [10,11], and other control methods are proposed. Among them, the backstepping method can simplify the controller design process of AUVs and is widely used [1,2].…”
Section: Introductionmentioning
confidence: 99%