This paper develops a new model reference adaptive control (MRAC) framework using partial-state feedback for solving a multivariable adaptive output tracking problem. The developed MRAC scheme has full capability to d...
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In this article, a unique and innovative design for addressing the speed synchronization problem in a multi-motor system using Brush less DC (BLDC), motors is presented by utilizing motor back emf equation and rotor p...
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We present an approach for combining standard recursive least squares based regression with proven direct model reference adaptive control using a recursively updated modification term. This approach is applicable to ...
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ISBN:
(纸本)9781424474264
We present an approach for combining standard recursive least squares based regression with proven direct model reference adaptive control using a recursively updated modification term. This approach is applicable to adaptivecontrol problems where the uncertainty can be linearly parameterized. The combined training law drives the adaptive weights smoothly to a recursively updated least squares estimate of the ideal weights and is shown to have a stability proof. Expected improvement in performance of the adaptive law is validated through simulation.
This paper introduces an optimal consensus control scheme for nonlinear multi-agent systems with completely unknown dynamics. In general, it is difficult to solve the coupled Hamilton-Jacobi-Bellman(HJB) equations, ...
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This paper introduces an optimal consensus control scheme for nonlinear multi-agent systems with completely unknown dynamics. In general, it is difficult to solve the coupled Hamilton-Jacobi-Bellman(HJB) equations, which the optimal consensus control relies on in multi-agent systems, especially unknown nonlinear systems. For the purpose of solving the problem, we propose an optimal consensus control approach based on the model reference adaptive control(MRAC) and adaptive dynamic programming(ADP). Using the structure of the diagonal recurrent neural network, the identifier and controller are devised to achieve MRAC for every plant of the unknown nonlinear systems, i.e. the referencemodel serves as a dynamic model of each individual agent. Then, according to referencemodels of distributed agents, an adaptive dynamic programming(ADP)is introduced to approximate the solution of the coupled HJB equations.
Designing missile autopilots is a challenging problem due to highly nonlinear uncertain aerodynamics, and stringent performance requirements. In this paper a robust adaptive augmenting controller is designed for a gen...
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ISBN:
(纸本)9781467386838
Designing missile autopilots is a challenging problem due to highly nonlinear uncertain aerodynamics, and stringent performance requirements. In this paper a robust adaptive augmenting controller is designed for a generic non-minimum phase pitch-axis missile autopilot. The control system consists of a robust L2 gain optimal controller as a baseline and an incremental robust direct model reference adaptive control (MRAC). The baseline controller is designed using robust convex programming covering multiple operating regions. The main objective of designing a retrofit adaptivecontroller is to provide strong robust performance in presence of uncertainties such as parametric uncertainties, reduced control effectiveness, etc. Simulation tests are performed to assess stability and performance of nonlinear closed-loop adaptive system in presence of uncertainties in pitching moment and normal force coefficients, unmodeled time-delays, and variations in Mach number. In addition, results in simulations indicate satisfactory robustness in case of severe loss of control effectiveness event and uncertainty in pitch aerodynamic model.
We apply a recently developed method of adaptivecontrol known as Extremum Seeking model reference adaptive control (ES-MRAC) to a hypersonic vehicle model. The system under consideration is a two input, two output no...
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ISBN:
(纸本)9781479978878
We apply a recently developed method of adaptivecontrol known as Extremum Seeking model reference adaptive control (ES-MRAC) to a hypersonic vehicle model. The system under consideration is a two input, two output nonlinear model of a hypersonic vehicle. The method is based on the use of extremum seeking (ES) optimization for adaptation. Instead of deriving an adaptation law as in mainstream adaptivecontrol methods, ES-MRAC calculates the update law in real-time. We investigate the behavior of the method in simulations.
Two typical methods for model reference adaptive control are introduced. By integrating the Narendra adaptivecontrol method and the variable structure model reference adaptive control method, a new variable model ref...
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A modelreferencecontrol system presented by Hori et al. (1989) is applied to an electrohydraulic servo system and simulations are carried out to study how the performance of a controller changes depending upon how t...
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ISBN:
(纸本)0852965095
A modelreferencecontrol system presented by Hori et al. (1989) is applied to an electrohydraulic servo system and simulations are carried out to study how the performance of a controller changes depending upon how the stable sampling zeros are handled. An adaptive version of this control scheme is also studied. Experimental results confirm the simulation study.< >
This paper studies speed sensorless Direct Torque control (DTC) for 3-level inverter-fed induction motor using different observers. Indeed, the first part presents the DTC using 3-level inverter and the second part in...
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ISBN:
(纸本)9781538685167
This paper studies speed sensorless Direct Torque control (DTC) for 3-level inverter-fed induction motor using different observers. Indeed, the first part presents the DTC using 3-level inverter and the second part introduces three different observers: The modelreferenceadaptive System (MRAS), the adaptive Luenberger observer and the Extended Kalman Filter (EKF). The last part shows the simulation results of all sensorless DTC schemes carried under Matlab/Simulink and compares their performances over a wide speed range.
Non-minimum phase systems pose a challenge in the design of MRAC. While some methods that can handle non-minimum phase systems are available in the literature, it is not always easy to guarantee tracking performance w...
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ISBN:
(纸本)9781479978878
Non-minimum phase systems pose a challenge in the design of MRAC. While some methods that can handle non-minimum phase systems are available in the literature, it is not always easy to guarantee tracking performance with these methods. This paper offers a partial solution to this problem. The method of generating an augmented plant by adding some dynamics in parallel to the original plant is used to make the adaptation scheme see a minimum phase system. The drawback of this method is that the error between original plant and original referencemodel does not asymptotically converge to zero, and even analysis of this error is not available in the literature. This paper offers a way to find an upper bound on the tracking error and design an alternative referencemodel to minimize the error. The application of the new referencemodel leads to improved tracking performance with respect to the original referencemodel. The alternative referencemodel is designed by iteratively solving linear matrix inequalities. Performance guarantees are given in terms of an L_2-gain bound from the reference to the tracking error, and this L_2-gain bound is minimized when the matrix inequalities are solved. An aerospace example is given to illustrate the effectiveness of our approach.
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