Using the FACTS controllers, such as static synchronous compensator (STATCOM), as it provides continuous reactive power, in the grid including wind turbine (WT) equipped with doubly fed induction generator, for improving voltage profile (under normal circumstances) and providing a transition ability from inductor generator transition state has been proposed. In this paper, in order to contr...

This paper presents an attitude control algorithm for a Reusable Launch Vehicle (RLV) with a low lift/drag ratio (L/D < 0.5), in the presence of external disturbances, model uncertainties, control output constraints and the thruster model. The main novelty of proposed control strategy is a new combination of the attitude control methods included backstepping, dynamic inversion and adaptive cont...

This paper investigates state feedback control for a class of discrete-time multiple input and output nonlinear systems from the perspective model-free adaptive observation. The design dynamic can be efficiently carried out using linearization stability proposed method is guaranteed by theoretical analysis. Numerical simulation tests experimentation on continuous stirred tank reactor are to val...

This paper investigates the usage of some sophisticated and advanced nonlinear control algorithms inorder to control a nonlinear Coupled Tanks System. The first control procedure is called the Feedbacklinearisation control (FLC), this type of control has been found a successful in achieving a global exponentialasymptotic stability, with very short time response, no significant overshooting is r...

This paper deals a tracking trajectory controller design of a tricycle robot as a non-holonomic system with a piecewise multi-linear (PML) model. The approximated model is fully parametric. Input-output (I/O) dynamic feedback linearization is applied to stabilize PML control system. We also apply a method for a tracking control based on PML models to the tricycle robot. Although the controller ...

No AccessEngineering NotesReinforcement-Learning-Based Adaptive Optimal Flight Control with Output Feedback and Input ConstraintsBo Sun Erik-Jan van KampenBo https://orcid.org/0000-0002-5229-8545Delft University of Technology, 2629 HS Delft, The Netherlands*Ph.D. Student, Operations Department, Faculty Aerospace Engineering, South Holland.Search for more papers by this author Kampen https://orc...

In this paper, we design an H∞ controller for a class of lower-triangular time-delay systems. Backstepping is applied to construct an explicit feedback controller, and the closed-loop system maintains internal stability and an L2-gain from the disturbance input to the output. The design is delay-dependent. Simulations on an example system demonstrate the good performance of the proposed design....