Higher order sliding mode controller design for a research nuclear reactor considering the effect of xenon concentration during load following operation

2015 ◽  
Vol 75 ◽  
pp. 728-735 ◽  
Author(s):  
G.R. Ansarifar ◽  
M. Rafiei
Keyword(s):  
Nuclear Reactor ◽  
Controller Design ◽  
Sliding Mode ◽  
Higher Order ◽  
Sliding Mode Controller ◽  
Load Following ◽  
Xenon Concentration ◽  
Research Nuclear Reactor

Model validation and higher order sliding mode controller design for a research reactor

2009 ◽  
Vol 36 (1) ◽  
pp. 37-45 ◽  
Author(s):  
S.H. Qaiser ◽  
A.I. Bhatti ◽  
Masood Iqbal ◽  
R. Samar ◽  
J. Qadir
Keyword(s):  
Model Validation ◽  
Research Reactor ◽  
Controller Design ◽  
Sliding Mode ◽  
Higher Order ◽  
Sliding Mode Controller

T-S fuzzy-based sliding mode controller design for discrete-time nonlinear model and its applications

2020 ◽  
Vol 519 ◽  
pp. 183-199 ◽  
Author(s):  
Ramasamy Subramaniam ◽  
Dongran Song ◽  
Young Hoon Joo
Keyword(s):  
Nonlinear Model ◽  
Discrete Time ◽  
Controller Design ◽  
Sliding Mode ◽  
Sliding Mode Controller

scholarly journals Adaptive Multivariable Super-Twisting Sliding Mode Controller and Disturbance Observer Design for Hypersonic Vehicle

2016 ◽  
Vol 2016 ◽  
pp. 1-9 ◽  
Author(s):  
Wenru Fan ◽  
Bailing Tian
Keyword(s):  
Disturbance Observer ◽  
Controller Design ◽  
Sliding Mode ◽  
Hypersonic Vehicle ◽  
Observer Design ◽  
Sliding Mode Controller ◽  
Finite Time Convergence ◽  
Gain Adaptation ◽  
Chattering Reduction ◽  
Sliding Manifold

A multivariable super-twisting sliding mode controller and disturbance observer with gain adaptation, chattering reduction, and finite time convergence are proposed for a generic hypersonic vehicle where the boundary of aerodynamic uncertainties exists but is unknown. Firstly, an input-output linearization model is constructed for the purpose of controller design. Then, the sliding manifold is designed based on the homogeneity theory. Furthermore, an integrated adaptive multivariable super-twisting sliding mode controller and disturbance observer are designed in order to achieve the tracking for step changes in velocity and altitude. Finally, some simulation results are provided to verify the effectiveness of the proposed method.

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