Results 251 to 260 of about 17,161,577 (311)
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IEEE/ASME transactions on mechatronics, 2019
The lateral and longitudinal stability is important and difficult for a distributed drive electric vehicle (DDEV). Current control methods for the lateral and longitudinal stability are designed based on the static model and parameter without considering
Ke Shi +3 more
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The lateral and longitudinal stability is important and difficult for a distributed drive electric vehicle (DDEV). Current control methods for the lateral and longitudinal stability are designed based on the static model and parameter without considering
Ke Shi +3 more
semanticscholar +1 more source
Decoupled Control/Error Weighting for Predictive Control
Journal of Dynamic Systems, Measurement, and Control, 1993This paper presents a basic review and explanation of the predictive control, discusses the inherent inadequacies with the control/error weighting scheme employed by the predictive control, and recommends some modifications to greatly improve its performance.
T. R. Kurfess, D. E. Whitney
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Decoupled fuzzy sliding-mode control
IEEE Transactions on Fuzzy Systems, 1998A decoupled fuzzy sliding-mode controller design is proposed. The decoupled method provides a simple way to achieve asymptotic stability for a class of fourth-order nonlinear systems with only five fuzzy control rules. The ideas behind the controller are as follows. First, decouple the whole system into two second-order systems such that each subsystem
null Ji-Chang Lo, null Ya-Hui Kuo
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Decoupling non-sequential stochastic control problems
Systems & Control Letters, 1991zbMATH Open Web Interface contents unavailable due to conflicting licenses.
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Self‐tuning control with decoupling
AIChE Journal, 1987AbstractA new method to design adaptive, self‐tuning controllers is presented that incorporates decoupling for multivariable control problems. The algorithm is shown to result from two very different derivations. The first approach employs multiple single‐input/single‐output self‐tuning controllers but with a classical decoupling scheme incorporated ...
I‐Lung Chien +2 more
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New technique for decoupling control
International Journal of Systems Science, 1993Abstract A new technique for decoupling controller design is proposed. A reference model representing the desired closed-loop dynamic behaviour is chosen. A quadratic performance index is used to measure both coupling and tracking errors in the closed-loop system. The system state equation is organized in incremental canonical form.
Q. J. XIA, M. RAO, Y. X. SUN, Y. Q. YING
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Cost of cheap decoupled control
Proceedings of the 37th IEEE Conference on Decision and Control (Cat. No.98CH36171), 2002Although decoupling a controlled system increases costs in terms of some performance measures, it is often desirable from an applied perspective point of view. Here, the average quadratic tracking error is used to explicitly quantify decoupling costs allowing the relative desirability of decoupling for particular applications to be determined.
T.S. Brinsmead, G.C. Goodwin
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Achieving Decoupling with Predictive Controllers
1986 American Control Conference, 1986Predictive controllers such as Dynamic Matrix Control (DMC) and Internal Model Control (IMC) are formulated as true multivariable control systems rather than as traditional multiloop systems. For many processes such predictive controllers perform well with a minimum of interaction between controlled variables.
Paul R. Maurath +2 more
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Decoupling control of vehicle chassis system based on neural network inverse system
Mechanical systems and signal processing, 2018Steering and suspension are two important subsystems affecting the handling stability and riding comfort of the chassis system. In order to avoid the interference and coupling of the control channels between active front steering (AFS) and active ...
Chunyan Wang +4 more
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Structural design and decoupled control
Acta Astronautica, 1989Abstract The decoupled control of an optimally designed space structure is considered. The optimal structure is a derivative of the CSDL I model spacecraft. In particular, the effects of structural perturbations on the optimal design are considered. The stiffness matrix for the structure is perturbed by changing the areas of its rod members.
Robert A. Calico, Franklin E. Eastep
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