2020
DOI: 10.1007/978-3-030-36621-6_5
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Constrained Sliding-Mode Control: A Survey

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Cited by 7 publications
(3 citation statements)
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“…where y, z, and đ›Œ respectively denote horizontal, vertical, and angular displacements, g is the gravitational acceleration, d ∈ R 3×1 is the vector of lumped force and moment disturbances, and the net thrust and moment acting on the fixed-rotor helicopter are proportional to inputs u 1 and u 2 . In this problem, the input constraints are |u 1 | < 10 m∕s 2 and |u 2 | < 20 rad∕s 2 .…”
Section: Simulation Studymentioning
confidence: 99%
See 1 more Smart Citation
“…where y, z, and đ›Œ respectively denote horizontal, vertical, and angular displacements, g is the gravitational acceleration, d ∈ R 3×1 is the vector of lumped force and moment disturbances, and the net thrust and moment acting on the fixed-rotor helicopter are proportional to inputs u 1 and u 2 . In this problem, the input constraints are |u 1 | < 10 m∕s 2 and |u 2 | < 20 rad∕s 2 .…”
Section: Simulation Studymentioning
confidence: 99%
“…In control systems implementations, to prevent certain critical conditions associated with the violation of constraints, the use of safe control methods has become an increasingly common practice, 1,2 and several methodologies have been extended in order to cope with constraints. For instance, sliding‐mode control (SMC), a nonlinear control method valued for its properties of robustness versus relevant classes of uncertainties, 3,4 has been coupled with barrier functions to provide barrier function‐based SMC approaches capable of controlling state constrained dynamical systems 5‐8 .…”
Section: Introductionmentioning
confidence: 99%
“…In addition, it should be mentioned that constrained sliding-mode control is an active research area, and we are not considering it in the proposed work. However, for completeness, we refer the reader to [35,36,55,56]. x 1 (t) and y 1 (t)…”
Section: A Static Sliding Modementioning
confidence: 99%