Extensive effort in controller design of aircraft systems is invested ensuring safe, stable behavior in spite of large parametric uncertainties. Particular attention is placed on anomalous flight conditions harbored b...
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Extensive effort in controller design of aircraft systems is invested ensuring safe, stable behavior in spite of large parametric uncertainties. Particular attention is placed on anomalous flight conditions harbored by the atmosphere, especially icing. This paper presents a regulation trigger-based adaptivecontroller to cope with the impact of ice on the aircraft equations of motion and to control the aircraft pitch to the commanded angle. For a pitch model of an aircraft system with the impact of icing, the design of a stabilizing certainty-equivalence controller using backstepping is first given, and it is succeeded by the introduction of a regulation-triggered batch least-squares identifier. A theorem is incorporated that guarantees that 1) pitch angle and pitch rate converge to the setpoint asymptotically, and 2) parameter estimates end after a finite number of switches. Finally, simulation results of an aircraft experiencing icing demonstrate the effectiveness of the identifier, with the trajectory of the iced system using the proposed identifier closely following that of the nominal system.
In this paper, an optimal multi-adaptive robust controller is proposed for robot manipulators using the gradient descent method and artificial bee colony. At first, model reference adaptive control (MRAC) and sliding ...
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In this paper, an optimal multi-adaptive robust controller is proposed for robot manipulators using the gradient descent method and artificial bee colony. At first, model reference adaptive control (MRAC) and sliding mode control (SMC) are separately designed for handling a robot manipulator with two revolute (2R) joints. Further, the coefficients of the sliding surfaces and control efforts are updated via a suitable adaptive mechanism based on the gradient descent method. In addition, to minimize the weighted summation of integral time absolute error (ITAE), some constant parameters of the controllers are determined by the artificial bee colony optimization algorithm. Finally, comparisons and performance tests are illustrated to demonstrate the effectiveness and superiority of the proposed control scheme for trajectory tracking in comparison with other traditional approaches.
In this paper, a model-free data-driven prescribedtime-performance (DDPTP) algorithm is developed for the underactuated autonomous surface vehicle (ASV). By defining a leader to provide the dynamic reference signal, t...
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DC motors have wide acceptance in industries due to their high efficiency, low costs, and flexibility. The paper presents the unique design concept of a multi-objective optimized proportional-integral-derivative (PID)...
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DC motors have wide acceptance in industries due to their high efficiency, low costs, and flexibility. The paper presents the unique design concept of a multi-objective optimized proportional-integral-derivative (PID) controller and model reference adaptive control (MRAC) based controllers for effective speed control of the DC motor system. The study aims to optimize PID parameters for speed control of a DC motor, emphasizing minimizing both settling time (T-s) and % overshoot (% OS) of the closed-loop response. The PID controller is designed using the Ziegler Nichols (ZN) method primarily subjected to Taguchi-grey relational analysis to handle multiple quality characteristics. Here, the Taguchi L9 orthogonal array is defined to find the process parameters that affect T-s and % OS. The analysis of variance shows that the most significant factor affecting T-s and % OS is the derivative gain term. The result also demonstrates that the proposed Taguchi-GRA optimized controller reduces T-s and % OS drastically compared to the ZN-tuned PID controller. This study also uses MRAC schemes using the MIT rule, Lyapunov rule, and a modified MIT rule. The DC motor speed tracking performance is analyzed by varying the adaptation gain and reference signal amplitude. The results also revealed that the proposed MRAC schemes provide desired closed-loop performance in real-time in the presence of disturbance and varying plant parameters. The study provides additional insights into using a modified MIT rule and the Lyapunov rule in protecting the response from signal amplitude dependence and the assurance of a stable adaptivecontroller, respectively.
This work proposes a solution for the adaptive stabilization of second-order linear systems with unknown parameters using only position measurements. Only the sign of the control law is known and the system is affecte...
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This work proposes a solution for the adaptive stabilization of second-order linear systems with unknown parameters using only position measurements. Only the sign of the control law is known and the system is affected by constant perturbations. The crux of the proposed control scheme the use of an alternative representation of the system obtained through integrating over time the original system representation. In this way, the whole state of the alternative representation is available from measurements, and an extended state space representation is obtained through the alternative representation and the differential equation related to the integral over time of the original input. Later, an adaptivecontrol methodology and an backstepping procedure are used to establish closed-loop stability. Simulation results support the findings. (C) 2020 European control Association. Published by Elsevier Ltd. All rights reserved.
This paper develops a neural-network-based model reference adaptive control (MRAC) scheme for a rotorcraft in the presence of input saturation. Such a control scheme provides acceptable tracking performance for the ro...
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This paper develops a neural-network-based model reference adaptive control (MRAC) scheme for a rotorcraft in the presence of input saturation. Such a control scheme provides acceptable tracking performance for the rotorcraft in a wide range of flight conditions. Combined with hyperbolic tangent functions, the MRAC scheme is capable of tracking the reference signals without violating input constraints. A modified projection operator is utilized to prevent system from parameter drift due to the strong nonlinearity and uncertainty of the rotorcraft mathematical model. Stability of the proposed MRAC scheme is proved based on Lyapunov stability theory. The performance of the resulting controller is tested by conducting numerical simulations for an autonomous rotorcraft in various flight missions. (C) 2021 ISA. Published by Elsevier Ltd. All rights reserved.
This paper studies a class of coupled dynamical systems consisting of an actuated dynamical system interconnected with an unactuated dynamical system. The actuated dynamical system is considered to have a measurable s...
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This paper studies a class of coupled dynamical systems consisting of an actuated dynamical system interconnected with an unactuated dynamical system. The actuated dynamical system is considered to have a measurable state for feedback control, whereas only the output is available from the unactuated dynamical system. Specifically, the control objective for this class of dynamical systems is to allow a desired subset of the state of the actuated dynamical system to follow given commands in the presence of uncertain parameters and unactuated dynamical system coupling. To this end, our contribution is a mixed state and output feedback framework in the context of model reference adaptive control, which is predicated on integrated nominal and adaptivecontrol laws. The key feature of the proposed model reference adaptive control architecture is to guarantee stability of the closed-loop coupled dynamical system as well as to assign user-defined bounds on system error trajectories utilised by the adaptivecontrol law for achieving a prescribed level of overall system performance.
In this study, closed-loop flow control is implemented in order to attenuate the lift fluctuation of a circular cylinder oscillating harmonically in a uniform stream. Through the numerical simulation of the incompress...
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An adaptivecontrol is proposed for H∞ tracking of uncertain dynamical systems. A referencemodel which achieves a robust tracking in the presence of L2 disturbances is introduced by using H∞ control with transients...
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This paper presents a novel hyperstability-based adaptivecontrol strategy for induction motors, distinguishing itself from conventional model reference adaptive control (MRAC) approaches by integrating enhanced robus...
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