This paper presents how MaTX is used to aid the education of Classical and Modern control Theory in a lecture named system Engineering Practice for third year students at Department of computers and system Engineering...
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This paper presents how MaTX is used to aid the education of Classical and Modern control Theory in a lecture named system Engineering Practice for third year students at Department of computers and system Engineering, College of Science and Engineering, Tokyo Denki University, Japan.
In this paper we describe a Matlab toolbox for modeling, analysis, and controldesign for multidimensional systems. The software may be obtained from the author's home page.
In this paper we describe a Matlab toolbox for modeling, analysis, and controldesign for multidimensional systems. The software may be obtained from the author's home page.
CONDUIT is a computer software package. Its purpose is to assist engineers in the design of aircraft controlsystems. It is menu-driven, interactive, and based on previously developed general software for optimization...
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CONDUIT is a computer software package. Its purpose is to assist engineers in the design of aircraft controlsystems. It is menu-driven, interactive, and based on previously developed general software for optimization-based computer-aideddesign. CONDUIT is presently being used to assist in the design of stability and control augmentation systems at ten organizations.
Applied Dynamics has developed a methodology to be used to build bridges between computeraidedcontrolsystemdesign (CACSD) and Embedded Software Development (ESD) toolsets. This methodology consists of a software-d...
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Applied Dynamics has developed a methodology to be used to build bridges between computeraidedcontrolsystemdesign (CACSD) and Embedded Software Development (ESD) toolsets. This methodology consists of a software-design level layered on top of the CACSD modeling layer. The methodology has its initial realization as a tool that converts a controller algorithm in Mathworks' Simulink and Stateflow CACSD toolset into a controller implementation in Applied Dynamics' BEACON ESD toolset.
A theoretical approach and applied techniques for designing analogues engineering devices and systems with due account of random variations in system parameters and reliability specifications are considered. For solvi...
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A theoretical approach and applied techniques for designing analogues engineering devices and systems with due account of random variations in system parameters and reliability specifications are considered. For solving this problem a so-called operational/parametric approach is used. This approach is based on the computer-aided simulation of system capability and availability, parameter deviations and techniques of optimal parametric synthesis in terms of reliability criteria. Special attention is paid to algorithms that reduce the labor content of parameters optimization problems. For seeking a numerical solution of the parametric design problem a computer-aided reliability-oriented designsystem is proposed.
Although it has been considered that a transfer function based method is difficult to use to treat multi-input, multi-output (MIMO) systems, the MIMO controlsystem can be treated in a comparatively easy way using a c...
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Although it has been considered that a transfer function based method is difficult to use to treat multi-input, multi-output (MIMO) systems, the MIMO controlsystem can be treated in a comparatively easy way using a characteristic transfer function matrix (CTFM) concept. In this paper, based on properties of the CTFM, a computeraided technique is presented for deriving the class of realizable transfer function matrices of a controlsystem for a prescribed order controller. Then the possibility as a practical design tool is discussed.
The complete environment available for the Concept to Code process is described. This process is illustrated using an example of an automatic transmission. The problem posed is: 'design a system which will shift t...
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The complete environment available for the Concept to Code process is described. This process is illustrated using an example of an automatic transmission. The problem posed is: 'design a system which will shift through the gears of a vehicle based on throttle input.'
The high computation and visualization power now available at the control engineer's desk opens the perspective of embedding CACSD Technology into a Virtual Engineering environment. This enables concurrent interac...
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The high computation and visualization power now available at the control engineer's desk opens the perspective of embedding CACSD Technology into a Virtual Engineering environment. This enables concurrent interaction of control engineering with multidisciplinary high-fidelity system dynamics modeling, and supports a fundamental change of the conventional controldesign tuning process in a computation framework of fast nonlinear simulation, automatic search for feasible solutions, and interactive multiobjective optimization to trade-off conflicting design requirements. Such an environment promotes active decision support to foster the control engineer's role as the prime decision maker in system dynamics design.
In this paper, a fuzzy-neuro approach will be presented for the design of bang-bang controlsystem. A description of the architecture will be given. The multi-layered structure of the controller is essentially a neura...
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In this paper, a fuzzy-neuro approach will be presented for the design of bang-bang controlsystem. A description of the architecture will be given. The multi-layered structure of the controller is essentially a neural network which resembles a fuzzy rule-based system. The robustness issue of an application to a heating system will also be described.
The paper describes a systematic computer-aideddesign procedure for Failure Detection and Identification (FDI) and Adaptive Reconfigurable control (ARC) for aerospace applications. The overall approach is based on a ...
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The paper describes a systematic computer-aideddesign procedure for Failure Detection and Identification (FDI) and Adaptive Reconfigurable control (ARC) for aerospace applications. The overall approach is based on a Decentralized FDI-ARC scheme integrating separate modules for sensor, control effector and engine FDI with that for structural damage FDI. One of the important issues in this context is information exchange among the modules. In the paper we focus on the module for FDI-ARC in the presence of control effector failures, and describe our approach as well as future work in this area.
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