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The good current tracking, flexible control design or reduced switching losses are some of the benefits that explain the recently increased attention on finite-control-set model predictive control.
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Up to now, dissipativity has attracted many researchers' attention because it does not only unifies the (H_{infty }) and passivity performance [30 35] but also provides a more flexible robust control design in practical engineering, such as chemical process control [36] and power converters [37].
In comparison with previous studies, this work allows strip design with freeform developable patches, generates better results in the surface assessment, and provides more flexible control on the design shape.
To achieve different control objectives as well as remain the properties of VSG, the proposed flexible control strategy is designed as a cascaded control framework, which mainly includes four modules: basic VSG algorithm, a novel CRG, an innovative PRG, and a typical current regulator.
Thirdly, a horizon-1 predictive controller based on flexible control Lyapunov functions is designed for the resulting model with polytopic uncertainty and hard constraints.
Thirdly, a robust predictive controller based on flexible control Lyapunov functions is designed, which explicitly takes into account the bounds of the disturbances caused by time-varying delays and guarantees also the input-to-state stability of the system in a non-conservative way.
The flying-capacitor multilevel inverter is a recently developed topology to ensure a flexible control and a modular design.
This paper presents the so called Direct Feedback Linearization (DFL) technique as a simple and flexible method for nonlinear control design.
Simulation results satisfy the basic idea that floating voltage can ensure a flexible control and a modular design of flying-capacitor multilevel inverter.
This paper presents a research activity on the design of an Integrated Control Structure framework enabling to ensure co-jointly structure sizing and robust control design for flexible satellite.
In this paper, we investigate the problem of attitude control design for flexible spacecraft with external disturbance, input magnitude and rate constraints.
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