In this study, model reference adaptive control algorithm with successive approximation method is suggested for nonlinear systems. The proposed method uses Linear Time Varying (LTV) approximations of the nonlinear mod...
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In this study, model reference adaptive control algorithm with successive approximation method is suggested for nonlinear systems. The proposed method uses Linear Time Varying (LTV) approximations of the nonlinear model to design the controller. Provided that an adaptivecontrol exists for the approximated LTV system, it is shown that the responses of the approximated LTV systems converge to the response of the nonlinear system. Then the model reference adaptive control for nonlinear system is designed by using successive LTV approximations. The proposed control design method is exemplified with a nonlinear dynamical system.
Paper presents the model reference adaptive control applied for the glucose concentration control in Type 1 diabetes mellitus (T1DM) subject. The adaptivecontroller structure allows to present the commanded insulin i...
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Aeroengine is a kind of multi-variable controlled object with strong nonlinearity and coupling, which is usually difficult to be described by precise mathematical models. Aiming at the condition that near the aeroengi...
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ISBN:
(纸本)9781479970186
Aeroengine is a kind of multi-variable controlled object with strong nonlinearity and coupling, which is usually difficult to be described by precise mathematical models. Aiming at the condition that near the aeroengine's stable operating points, model parameters are unknown but unchanged with time, this thesis designs aeroengine model reference adaptive control system based on the Lyapunov stability theory, by choosing Lyapunov function, in the case of keeping the system stable, the adaptive parameter adjustment law is obtained. Last but not least, this thesis proposes improvement measures to deal with the shaking rotating speed problem of the aeroengine model reference adaptive control system as the use of the Lyapunov method. By simulation experiments, the results prove that the designed control system can realize adaptive state tracking control of aeroengine, and as well meet the performance index requirements for the aeroengine's control system.
Safety is the most fundamental problem of safety-critical systems. Safety control addresses the problem whether a given unsafe region of the state space can be avoided by a specific control-input. Moreover, linearly p...
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Safety is the most fundamental problem of safety-critical systems. Safety control addresses the problem whether a given unsafe region of the state space can be avoided by a specific control-input. Moreover, linearly parameterized dynamical system is a general assumption in most safety-critical adaptivecontrol literature;however, unknown parameters in real systems are usually nonlinear. The control problem of nonlinearly parameterized systems is really difficult without linear-in-the-parameters (LIP) assumptions, which tends to be complicated and computationally intensive. In this paper, a novel modelreference safety-critical adaptivecontrol (MRAC) approach is proposed for a class of nonlinearly parameterized systems. The proposed approach involves a novel controller architecture with a modified update law, which specifically filters out the unsafe behavior (the system is in a state which the system cannot operate normally, i.e., the given unsafe region), while preserving favorable tracking capability and robustness. The novelty of this paper is that the nonlinearly parameterized systems can be enforced safety, without LIP assumptions and complex calculations. Most importantly, this approach is effective for nonlinearly parameterized systems as well as linearly parameterized systems. Finally, three illustrative numerical examples are presented to demonstrate the effectiveness of the proposed design approach.
The method [K]control of adaptive Multiple-timescale Systems (KAMS) has been used as a method of adaptivecontrol for systems with states that evolve at vastly different rates and with uncertain parameters. Prior rese...
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In this paper, we report a new adaptivemodelreferencecontrol algorithm for a class of DC-AC inverters. The proposed design is based on a simplified discrete-time domain model with completely unknown system and inpu...
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This paper studies reference tracking control of uncertain lateral vehicle dynamics, using a blending based multiple-model reference adaptive control (MMRAC) approach to overcome the parametric uncertainties and time-...
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Techniques known as Nonlinear Set Membership prediction, Lipschitz Interpolation or Kinky Inference are approaches to machine learning that utilise presupposed Lipschitz properties to compute inferences over unobserve...
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In order to obtain better static and dynamic performance of the nonlinear system, in this paper the compound control system which the inner loop adopted direct inverse modelcontrol and the outer loop adopted model re...
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In order to obtain better static and dynamic performance of the nonlinear system, in this paper the compound control system which the inner loop adopted direct inverse modelcontrol and the outer loop adopted model reference adaptive control was designed. Aiming at the difficulty to building inverse model in the inverse modelcontrol system in inner loop, the modeling method of inverse model based on the LSVM is proposed. As seen from the simulation results that the actual output signal is in good agreement with the desired output. It is show that the model reference adaptive control system based on LSVM inverse model has a good ability to control nonlinear object with high tracking precision, good dynamic performance and better control effect
This paper presents a tracking error convergence proof for the multi-input multi-output direct model reference adaptive control problem. The proof is valid for square plants that are potentially nonminimum phase. This...
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ISBN:
(纸本)9781479978878
This paper presents a tracking error convergence proof for the multi-input multi-output direct model reference adaptive control problem. The proof is valid for square plants that are potentially nonminimum phase. This work is an extension of the surrogate tracking error adaptivecontrol techniques previously developed, though the assumed plant structure is altered to accommodate a wider range of dynamics. Error convergence is demonstrated using a composite system construction with Lyapunov stability techniques. The performance of the proposed control design is demonstrated through simulation of a linear version of an aircraft wing's aeroelasitc pitch and plunge dynamics.
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