This paper addresses the problem of robust control of spatially interconnected systems (SISs) subject to both exogenous disturbances and time-varying norm-bounded parameter uncertainties. A sufficient condition to the...
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ISBN:
(纸本)9781612848006
This paper addresses the problem of robust control of spatially interconnected systems (SISs) subject to both exogenous disturbances and time-varying norm-bounded parameter uncertainties. A sufficient condition to the well-posedness, stability and attractiveness of an SIS with respect to all admissible uncertainties is presented in terms of a set of matrix inequalities. For the synthesis of distributed dynamic output feedback controllers, the nominal system is expanded in its output space so as to eliminate the uncertainties in the system matrices. In reference to the standard distributed scaled H_(infinity) control, the synthesis of distributed robust H_(infinity) controllers is proposed based on the system model in the expanded space. Numerical examples validate the effectiveness of the method.
In this paper, an adaptive neural network (NN) control design is proposed for a class of parabolic partial differential equation (PDE) systems with boundary control actuation and unknown nonlinearities. Initially, app...
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In this paper, an adaptive neural network (NN) control design is proposed for a class of parabolic partial differential equation (PDE) systems with boundary control actuation and unknown nonlinearities. Initially, applying the Galerkin's method, the PDE system is represented by a finite-dimensional slow subsystem and a coupled infinite-dimensional fast residual subsystem. Subsequently, a modal-feedback controller is designed according to dissipative theory and small gain theorem, such that the closed-loop PDE system is practically stable. In the proposed boundary control scheme, a radial basis function (RBF) NN is employed to approximate the unknown nonlinearities of the slow subsystem. The outcome of the control problem is formulated as a linear matrix inequality (LMI) problem. Finally, the proposed design method is applied to the control of the temperature profile of a catalytic rod to illustrate its effectiveness.
This paper considers the problem of optimal control for the longitudinal model of a generic air-breathing hypersonic vehicle (AHV). Existing works about the optimal control of AHV usually require the complete knowledg...
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This paper considers the problem of optimal control for the longitudinal model of a generic air-breathing hypersonic vehicle (AHV). Existing works about the optimal control of AHV usually require the complete knowledge of the system dynamics. However, for realistic control systems, the dynamics may often be unknown or partially unknown, which makes it more difficult to handle the optimal controller design of the AHV. To overcome this difficulty, we propose an adaptive optimal controller synthesis algorithm, where the algebraic Riccati equation (ARE) is solved online without requiring the internal dynamics of AHV. control inputs for the AHV include the elevator deflection and the throttle setting. The simulation results on the AHV demonstrate the effectiveness of the proposed design method.
This paper focuses on the problem of further relaxing stabilization conditions for the Roesser type discretetime 2-D T-S fuzzy system. A novel kind of non-PDC control scheme is proposed to stabilize the closed-loop 2-...
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This paper focuses on the problem of further relaxing stabilization conditions for the Roesser type discretetime 2-D T-S fuzzy system. A novel kind of non-PDC control scheme is proposed to stabilize the closed-loop 2-D T-S fuzzy system, and then less conservative stabilization conditions are developed by using a new non-quadratic Lyapunov function for the underlying 2-D T-S fuzzy system. For one flxed degree of the homogeneous polynomially parameter-dependent matrix, the conservatism could be further reduced by exploiting the algebraic property of fuzzy membership functions and the obtained stabilization conditions may asymptotically approach to exactness in a convergent sense. Moreover, there are no slack matrix variables introduced in the control synthesis, and hence the computational burden is less than the existing ones while the same or less conservative results could be obtained. A numerical example is also provided to illustrate the effectiveness of the proposed methods.
In this paper, a valid approach is successfully addressed to design the adaptive stabilizing control law for a class of high-order nonlinear systems with unknown control coefficients and in triangular form. For such c...
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In this paper, a valid approach is successfully addressed to design the adaptive stabilizing control law for a class of high-order nonlinear systems with unknown control coefficients and in triangular form. For such control systems, the state-feedback stabilizing control has been investigated recently under the assumption that the lower bounds of the control coefficients are precisely known. This paper removes such assumption, and gives the recursive design procedure of stabilizing control law by employing the approach of adding a power integrator together with adaptive technique to the appropriately defined unknown system parameters. The designed state-feedback adaptive control law, which vanishes at the origin, guarantees that the states of the closed-loop system are globally asymptotically stable, while all the other signals are uniformly bounded.
The stabilization problem is investigated for a class of time-delay high-order nonlinear systems. by the flexible way of adding a power integrator, the recursive design procedure of a continuous state-feedback control...
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The stabilization problem is investigated for a class of time-delay high-order nonlinear systems. by the flexible way of adding a power integrator, the recursive design procedure of a continuous state-feedback controller is derived, and globally asymptotic stability of the resulting closed-loop system is proven with the aid of the delicate construction of an appropriate Lyapunov-Krasovskii functional. Finally, a simulation example is given to illustrate the correctness of the theoretical result.
According to the strict aerodynamic heating environment in the reentry process, a new reentry trajectory planning method is presented. A reasonable Heat Flux Rate (HFR) curve is designed with the energy of the aircraf...
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There are more and more needs for surface contact works, such as polish, grinding, paint, inspection, etc., with robot manipulators in recent years. In this paper, to achieve high-speed and high-precision surface cont...
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This article is concerned with the UAV path re-planning problem to be solved by using a novel approach based on the hybrid of virtual force and A* search algorithm (HVFA). The formulation of the UAV path re-planning i...
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This article is concerned with the UAV path re-planning problem to be solved by using a novel approach based on the hybrid of virtual force and A* search algorithm (HVFA). The formulation of the UAV path re-planning is presented, and the hybrid system model of virtual force (VF) is given. The scheme of path re-planning is designed and the corresponding computational complexity is analyzed quantitatively. Simulation results prove the feasibility and usefulness of using HVFA for UAV path re-planning. Performance comparisons between the HVFA method and the fuzzy virtual force (FVF) method demonstrate that the proposed approach is fast enough to meet the real-time requirements of the online path planning problems.
As a kind of large metallurgy equipment, liquid iron tank was used more widely. This paper took 130t liquid iron tank as an example. Three dimensions solid model of liquid iron tank lifting lug was constructed by ANSY...
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As a kind of large metallurgy equipment, liquid iron tank was used more widely. This paper took 130t liquid iron tank as an example. Three dimensions solid model of liquid iron tank lifting lug was constructed by ANSYS software in this paper. Grid division, restriction, load and strength finite element analysis were also made on relevant computation model. The relevant equivalent stress distribution rule of liquid iron tank lifting lug was found. The position of maximum equivalent stress was found. Liquid iron tank lifting lug can satisfy the use demand under slow lifting up working condition was proved. This analysis provides a practical and effective research method for research the strength and reliability of liquid iron tank. It also provides a theory base for corporation to recast and design liquid iron tank.
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