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- W4367358439 abstract "To stabilize the trajectory of an unmanned aerial vehicle (UAV) quadrotor system, a nonlinear adaptive integral sliding mode controller based on the Reaching law is proposed in this paper. First, the mathematical model of the quadrotor was developed using the Newton-Euler formalism, and then the design of an ISMC with three different types of reaching laws (reaching law with constant rate, exponential reaching law, and reaching law with power rate) and an analysis of their properties were investigated in this work. The proposed controllers’ performances were evaluated using the MATLAB/Simulation environment. The simulation results indicate that the ISMC-based exponential reaching law ensures fast convergence of the sliding manifold and attenuates the chattering phenomena in the sliding phase." @default.
- W4367358439 created "2023-04-30" @default.
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- W4367358439 date "2023-01-01" @default.
- W4367358439 modified "2023-09-26" @default.
- W4367358439 title "Design of an Integral Sliding Mode Control Based on Reaching Law for Trajectory Tracking of a Quadrotor System" @default.
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- W4367358439 doi "https://doi.org/10.1007/978-3-031-29857-8_85" @default.
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