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dc.contributor.authorZhu, Bing
dc.contributor.authorChen, Mou
dc.contributor.authorLi, Tao
dc.date.accessioned2022-02-04T22:14:29Z
dc.date.available2022-02-04T22:14:29Z
dc.date.copyright7/23/2020 12:00:00 AM
dc.date.issued2020
dc.identifier.issn0022-0434
dc.identifier.othermd_143_1_011708.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4275164
dc.description.abstractIn this paper, a trajectory tracking control scheme for a quadrotor unmanned aerial vehicle (UAV) under unknown external disturbance and input saturation is developed. This scheme includes the position control system and attitude control one, in which the attitude control system is further divided into the fast loop for angular velocity and the slow one for attitude angle based on time-scale separation principle. Then, an input constrained dynamic surface control scheme combined with a disturbance observer is designed to achieve the total thrust, desired roll, and pitch angle in the position control system. For the coupled attitude system, a dynamic surface control scheme together with generalized model predictive controller (GMPC) is proposed to tackle both the fast loop system and the slow one. Since the unknown external disturbance and input saturation are considered, a sliding mode disturbance observer (SMDO) is further designed to achieve the strong robustness. Finally, some simulation results are presented to show robustness and effectiveness of our proposed tracking scheme.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleRobust Constrained Trajectory Tracking Control for Quadrotor Unmanned Aerial Vehicle Based on Disturbance Observers
dc.typeJournal Paper
dc.journal.volume142
dc.journal.issue11
dc.journal.titleJournal of Dynamic Systems, Measurement, and Control
dc.identifier.doi10.1115/1.4047692
dc.journal.fristpage0111002-1
dc.journal.lastpage0111002-13
dc.page13
dc.treeJournal of Dynamic Systems, Measurement, and Control:;2020:;volume( 142 ):;issue: 011
dc.contenttypeFulltext


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