Abstract In this paper, the change of the relative degree structure at the controllable equilibrium is discussed. In the neighborhood of the controllable equilibrium, all nonlinear systems are approximated to linear c...
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Abstract In this paper, the change of the relative degree structure at the controllable equilibrium is discussed. In the neighborhood of the controllable equilibrium, all nonlinear systems are approximated to linear controllable system. The gap between the original nonlinear system and approximate linear system appears as a change of the relative degree structure. By comparison of these two structures, the necessary and sufficient condition is derived in order for the equilibrium not to be singular point via the input-output linearization. Based on this result, the selection of the output function is proposed. Moreover the output design method for linear stable zero dynamics is proposed.
Abstract The objective of this paper is to present systematic methods for throwing motion control of underactuated robots. The Pendubot, an underactuated two-link planar robot, is investigated as a dynamic model of th...
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Abstract The objective of this paper is to present systematic methods for throwing motion control of underactuated robots. The Pendubot, an underactuated two-link planar robot, is investigated as a dynamic model of the superior limbs for imitation of human throwing motion whose models are fundamentally underactuated in nature. The controller is designed based on input-output linearization and output zeroing control since the Pendubot is not input-state linearizable. The originality of this paper is to intentionally destabilize the zero dynamics, a nonlinear dynamics which remains unobservable from the output when the partially linearized dynamics converges exponentially to zero, to generate dynamic acceleration of the ball. Exact analysis of ordinary differential equations guarantees the explosive instability of the zero dynamics. Numerical simulations confirm the effectiveness of the proposed control strategy.
Abstract The paper considers stability of nonlinear discrete-time system linearized by output feedback. The boundedness of the control signal inside the linearized closed-loop system is studied in the research present...
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Abstract The paper considers stability of nonlinear discrete-time system linearized by output feedback. The boundedness of the control signal inside the linearized closed-loop system is studied in the research presented in this article. The algorithm for determination of the region of admissible inputs of the closed-loop system ensuring bounded-input bounded-output behavior of the controlled model is introduced. Both static and dynamic output feedback linearization algorithms are examined. To make the research more clear, the main results and applicability of the theory presented in the paper are demonstrated on several examples.
Due to nonlinear coupling and complex fight dynamics,the control of hypersonic aircrafts is usually *** this paper,taking the longitudinal motion of a general air-breathing hypersonic aircraft as the controlled object...
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Due to nonlinear coupling and complex fight dynamics,the control of hypersonic aircrafts is usually *** this paper,taking the longitudinal motion of a general air-breathing hypersonic aircraft as the controlled object,we designed a sliding mode controller to control velocity and altitude tracking based on input-output *** velocity and altitude subsystems can be obtained by linearization and highest order derivatives of outputs in the two subsystems are designed to satisfy the sufficient and necessary condition of sliding mode control based on Lyapunov functions.A saturation function is used in the sliding mode controller to reduce chattering instead of the discontinuous sign *** is studied to validate that the controller based on sliding mode can make the aircraft system stable and meet the desired tracking performance.
Two non-linear control structures are considered for position control of an electrohydraulic actuator. The first control structure is derived from a direct near input-output (IO) linearization of the actuator model wi...
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Two non-linear control structures are considered for position control of an electrohydraulic actuator. The first control structure is derived from a direct near input-output (IO) linearization of the actuator model with position as output. The second control structure is a cascade of a near IO linearizing pressure force controller as an inner loop to a feedback plus feedforward outer-loop position controller. In the present paper, it is shown that the two control structures are theoretically equivalent. Then, it is highlighted that the equivalence can be exploited to extract a simple and intuitive tuning procedure for selecting the gains of one control structure from the gains of the other structure. This result is particularly useful for tuning the near IO linearizing position controller as the interpretation of its gains is obscured by the non-linear state transformation of the feedback linearization. Some numerical simulation and experimental results are included to demonstrate the identified tuning procedure.
The geometric function of the target path was used to define the tracking error, converting the path following problem under study into a problem of output regulation. An exponential stable tracking control law was th...
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ISBN:
(纸本)9781424451821
The geometric function of the target path was used to define the tracking error, converting the path following problem under study into a problem of output regulation. An exponential stable tracking control law was therefore derived adopting input-output linearization approach and back-stepping technique. Thanks to the exponentially decaying terms added to the desired geometric path, the singularity problem is avoided by adjusting relevant coefficients. Numerical simulation results show the effectiveness of the control scheme.
The partial feedback linearization is capable of expressing a complicated nonlinear system as a simple form for control. To get a proper linearized subsystem, it is most important to select a proper coordinate transfo...
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The partial feedback linearization is capable of expressing a complicated nonlinear system as a simple form for control. To get a proper linearized subsystem, it is most important to select a proper coordinate transformation. This paper plays a fundamental role in selecting the proper coordinate by revealing the system structure with respect to a relative degree. The relative degree is a key concept to treat the partial feedback linearization, especially, the input-output linearization of an input affine system. Using special functions of the state characterized in the relative degree, all functions are parameterized and classified according to their relative degrees. Applying the proposed parameterization to a coordinate transformation, the system structure with respect to relative degrees is revealed. Moreover using the input-output linearization with parameterized outputs, it is also shown that the internal dynamics of the partially linearized system is parameterized.
The geometric function of the target path was used to define the tracking error, converting the path following problem under study into a problem of output regulation. An exponential stable tracking control law was th...
详细信息
The geometric function of the target path was used to define the tracking error, converting the path following problem under study into a problem of output regulation. An exponential stable tracking control law was therefore derived adopting input-output linearization approach and back-stepping technique. Thanks to the exponentially decaying terms added to the desired geometric path, the singularity problem is avoided by adjusting relevant coefficients. Numerical simulation results show the effectiveness of the control scheme.
The geometric function of the target path was used to define the tracking error,converting the path following problem under study into a problem of output *** exponential stable tracking control law was therefore deri...
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The geometric function of the target path was used to define the tracking error,converting the path following problem under study into a problem of output *** exponential stable tracking control law was therefore derived adopting input-output linearization approach and back-stepping *** to the exponentially decaying terms added to the desired geometric path,the singularity problem is avoided by adjusting relevant coefficients. Numerical simulation results show the effectiveness of the control scheme.
This contribution presents a: new approach for the numeric computation of the input-output linearizing feedback law, which is obtained exactly in an analytical form. By using a state space embedding technique the nonl...
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This contribution presents a: new approach for the numeric computation of the input-output linearizing feedback law, which is obtained exactly in an analytical form. By using a state space embedding technique the nonlinear system to be controlled is described by a higher order system with solely polynomial nonlinearities. Consequently, the nonlinearities of this system can be represented by multivariable Legendre polynomials, so that the derivation of the input-output linearizing feedback controller can be accomplished using the operational matrices of multiplication and of differentiation for Legendre polynomials. (C) 2004 Elsevier Ltd. All rights reserved.
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