This paper proposes an anti-windup mechanism for a model reference adaptive control scheme subject to actuator saturation constraints. The proposed compensator has the same architecture as well known non-adaptive sche...
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ISBN:
(纸本)9781665467612
This paper proposes an anti-windup mechanism for a model reference adaptive control scheme subject to actuator saturation constraints. The proposed compensator has the same architecture as well known non-adaptive schemes, which rely on the assumption that the system model is known fairly accurately. This is in contrast to the adaptive nature of the controller, which assumes that the system (or parts of it) is unknown. The approach proposed here uses of an "estimate" of the system matrices for the anti-windup compensator formulation and modifies the adaptation laws that update the controller gains. It will be observed that if the (unknown) ideal control gain is reached, a type of "model recovery anti-windup" formulation is obtained. In addition, it is shown that if the ideal control signal eventually lies within the control constraints, then, under certain conditions, the system states will converge to those of the referencemodel as desired. The paper highlights the main challenges involved in the design of anti-windup compensators for model-referenceadaptivecontrol systems and demonstrates its success via a flight control simulation.
Existence of unknown time-delay in the systems is a drastic restriction that it can menace the stability criteria and even deteriorate the performance system. This undesired case would be more intensified if that the ...
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Existence of unknown time-delay in the systems is a drastic restriction that it can menace the stability criteria and even deteriorate the performance system. This undesired case would be more intensified if that the uncertain input nonlinearity effects are also considered. To handle the input nonlinearities effects (results in dead-zone and/or hysteresis phenomena) and also unknown time-delay in the chaotic systems, this paper presents an observer-based model reference adaptive control (MRAC) scheme for a class of unknown time-delay chaotic systems with disturbances. This new method is a delay-independent variable-structure control method which is integrated with an observer system. The main task of the proposed approach is to accomplish a perfect tracking procedure such that unknown parameters are adapted via output estimation error. Furthermore, stability of the closed-loop system is achieved by means of the Lyapunov stability theory. Finally, the proposed methods are applied to some famous chaotic systems to verify the effectiveness of the proposed methods.
This paper studies the distributed leader-follower output consensus problem for continuous-time uncertain multiagent linear systems with general input-output forms. Specifically, we extend the well-known output feedba...
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An adaptive disturbance rejection control scheme is developed for solving the wind turbulence compensation problem. The turbulence wind studied in this paper is based on the mutual switch of several dominant wind dire...
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An adaptive disturbance rejection control scheme is developed for solving the wind turbulence compensation problem. The turbulence wind studied in this paper is based on the mutual switch of several dominant wind directions. The linear models of aircraft under wind turbulence with different dominant directions are given. An adaptivecontroller is designed based on the model reference adaptive control when the aircraft encounters the wind turbulence in different dominant directions. Desired closed-loop system stabilization and output tracking have been proven. A simulation study on aircraft compensation has been presented to verify the effectiveness of our designed method.
作者:
Liu, Y.Jia, Y.Beihang Univ BUAA
Res Div 7 Beijing 100191 Peoples R China Beihang Univ BUAA
Dept Syst & Control Key Lab Math Informat & Behav Semant LMIB Minist EducSMSS Beijing 100191 Peoples R China
This study is devoted to the adaptive consensus problem of multi-agent systems with partly unknown parameters and bounded external disturbances, under the guidance of an active leader with a reference input signal. Fi...
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This study is devoted to the adaptive consensus problem of multi-agent systems with partly unknown parameters and bounded external disturbances, under the guidance of an active leader with a reference input signal. Firstly, a distributed adaptive protocol is proposed for the system without disturbances by adopting the model reference adaptive control method. Then it is extended to the disturbed system by adding an adaptive disturbance compensator, based on the estimated upper and lower bounds of unknown disturbance. For the above two cases, sufficient conditions are, respectively, given to ensure that all agents can eventually track the prescribed leader. A numerical simulation illustrates the effectiveness of the proposed adaptive consensus protocol.
This research develops a dynamics and control framework for an unmanned powered parachute system. The 6 DOF dynamics are derived from the first principle/fundamentals. The dynamic equations are simulated and validated...
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ISBN:
(纸本)9780791886281
This research develops a dynamics and control framework for an unmanned powered parachute system. The 6 DOF dynamics are derived from the first principle/fundamentals. The dynamic equations are simulated and validated within the MATLAB Simulink simulation environment. A model reference adaptive controller algorithm is utilized and simulated to update coefficients to control the plant more accurately. A Computational Fluid Dynamics (CFD) simulation using SimScale is used to estimate aerodynamic coefficients. This paper is presented as a building block/work in progress for future work on robust and efficient adaptivecontrol of powered parachute aerial vehicles. Derivation of the dynamic equations is included in section two, while section three covers methods used to computationally define key aerodynamic coefficients and describe PPC simulation within the MATLAB Simulink environment. Finally, section four presents the results. Further research into this framework will include validating results through experimentation of the PPC aircraft and comparing dynamic model accuracy. Finally, more advanced control techniques will be applied to the PPC model in simulations and experiments.
We demonstrate how the transient response of model reference adaptive control (MRAC) is improved by utilizing Generalized Dynamic Inversion (GDI) and the corresponding nullspace parametrization in the powerful Grevill...
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We demonstrate how the transient response of model reference adaptive control (MRAC) is improved by utilizing Generalized Dynamic Inversion (GDI) and the corresponding nullspace parametrization in the powerful Greville formula. The proposed approach neither alters the referencemodel structure, nor it modifies it through feedback. Rather, the proposed approach utilizes the control redundancy in matching the referencemodel for the purpose of designing an MRAC control law that yields good transient closed loop adaptivecontrol response. The adaptive GDI-MRAC control law is composed of two parts: a particular part that enforces the referencemodel dynamics, and an auxiliary part that is affine in a null control vector. The particular and the auxiliary parts of the adaptivecontrol law are confined in the range space of the transposed control matrix and its orthogonal complement nullspace, respectively. The null control vector is projected onto the nullspace of the control matrix via a null-projection matrix. Hence, the null control vector design does not interfere with the referencemodel following, yet it can be designed via state feedback to improve closed loop state transient response. An improved Lyapunov control function is used to design the adaptation gains such that asymptotic vanishing of the state error dynamics is guaranteed. Extensive simulations are conducted to demonstrate the efficacy of the proposed method. Copyright (C) 2022 The Authors.
Basic L1 adaptivecontroller [1] is considered to be an improved controller as compared to the traditional Direct and Indirect MRAC (model reference adaptive control). It is proposed to take advantage of the new B con...
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ISBN:
(纸本)9781665465076
Basic L1 adaptivecontroller [1] is considered to be an improved controller as compared to the traditional Direct and Indirect MRAC (model reference adaptive control). It is proposed to take advantage of the new B control method [2,3] which exhibits improved performances in the time and the frequency domain and integrate these methods. Preliminary comparisons of the transmissions of output to input, as well as to input and output plant disturbances show a definite improvement when integrating L1 control and B control which we name BL1 control.
This paper presents a direct model reference adaptive controller for single-input/single-output discrete-time (and thus sampled-data) systems that are possibly nonminimum phase. The adaptivecontrol algorithm requires...
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This paper presents a direct model reference adaptive controller for single-input/single-output discrete-time (and thus sampled-data) systems that are possibly nonminimum phase. The adaptivecontrol algorithm requires knowledge of the nonminimum-phase zeros of the transfer function from the control to the output. This controller uses a retrospective performance, which is a surrogate measure of the actual performance, and a cumulative retrospective cost function, which is minimized by a recursive-least-squares adaptation algorithm. This paper develops the retrospective cost model reference adaptive controller and analyzes its stability.
The application of deoiling hydrocyclone systems as the downstream of three-phase gravity separator (TPGS) systems is one of the most commonly deployed produced water treatment processes in offshore oil and gas produc...
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The application of deoiling hydrocyclone systems as the downstream of three-phase gravity separator (TPGS) systems is one of the most commonly deployed produced water treatment processes in offshore oil and gas production. Due to the compact system's complexity and tailor-made features, it is always challenging to develop some optimally coordinated control solution for the coupled hydrocyclone and TPGS systems. It is obvious that coordinated control can better fulfill legislative discharge regulation by robustly maintaining high separation efficiencies. This paper presents a new control solution for a set of integrated hydrocyclone and TPGS systems by applying an improved multi-variable model reference adaptive control (MV-MRAC) approach with the aim of achieving both asymptotic output tracking and unknown disturbance rejection. A robust MV-MRAC controller design is proposed based on a control parameterization derived from a factorization of a high-frequency gain matrix Kp=LDS as a product of three matrices, where L represents unity lower triangular, D=sign(D) represents diagonal, and S represents positive definite, and a teaching-learning-based optimization (TLBO) algorithm for optimizing the adaption rates. The developed solution is analyzed and compared with a commonly deployed PI control solution on a model that is derived from a lab-scale produced water treatment process. This simulation study demonstrates the promising potential of the proposed control solution compared with the currently deployed PI control solution.
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