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Proceedings. IEEE International Symposium on Computer Aided Control System Design

 

 

 

 

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MathML in Polynomial Toolbox for Matlab
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R. Hornych, Z. Hurak, M. Sebek
This paper reports on a useful application of MathML to web presentation and export/import of polynomial matrices from/to the Polynomial Toolbox for Matlab/spl trade/. Two Matlab functions are described that can be used both for high quality visualization of polynomial matrices on web and for data exchange between Polynomial Toolbox and other software packages that compute with polynomial matrices... hiện toàn bộ
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Robust /spl mu/-design of a disk drive servo system
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P.H. Petkov, D.-W. Gu, M.M. Konstantinov
In this paper we show the application of the SLICOT routines, for robust control system analysis and design, in a disk drive servo control system design. An uncertainty model of the system plant is first derived which contains eleven uncertain parameters including four resonance frequencies, four damping coefficients and three rigid body model parameters. The /spl mu/-synthesis and analysis method... hiện toàn bộ
#Robustness #Disk drives #Servomechanisms #Robust stability #Robust control #System analysis and design #Control systems #Nonlinear control systems #Servosystems #Uncertainty
Thiết kế bộ điều khiển lái xe điện đa mục tiêu Dịch bởi AI
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J.C. Zavala, P. Stewart, P.J. Fleming
Sự hiện diện của tính linh hoạt trong hệ thống truyền động ô tô, kết hợp với các yếu tố phi tuyến như độ chơi của bánh răng, dẫn đến việc xuất hiện một phản ứng dao động không mong muốn khi có sự thay đổi đột ngột trong tín hiệu ga. Dao động này thường có tần số thấp (khoảng 2 đến 5 kHz) và có thể đủ lớn để gây ra cảm giác khó chịu cho người lái xe cũng như sự thất vọng chủ quan về khả năng điều k... hiện toàn bộ
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LFT representation of a longitudinal perturbed aircraft model by flatness approach
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F. Cazaurang, L. Lavigne, B. Bergeon
In this paper, an linear fractional transformations (LFT) model representing, the dynamic of the gap between a nominal model and a perturbed model of a longitudinal aircraft fighter along a trajectory is given. The proposed approach is based on a simplified model used to determine a nominal trajectory and corresponding input. This simplified nonlinear model is a flat nonlinear system. As the measu... hiện toàn bộ
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Numerical software in SLICOT for low order controller design
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A. Varga
We describe the model and controller reduction software recently developed for the control and systems library SLICOT. Based on the latest algorithmic developments, a powerful collection of Fortran 77 subroutines has been implemented to cover the relative error and frequency-weighted model reduction, as well as special controller reduction approaches. The new model and controller reduction routine... hiện toàn bộ
#Mathematical model #Power system modeling #Control system synthesis #Software libraries #Algorithms #Error correction #Frequency #Reduced order systems #Power system reliability #Software tools
Designing model predictive controllers with prioritised constraints and objectives
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E.C. Kerrigan, J.M. Maciejowski
This paper shows how a class of objective functions can be incorporated into a prioritised, multiobjective optimisation problem, for which a solution can be obtained by solving a sequence of single-objective, constrained, convex programming problems. The objective functions considered in this paper typically arise in model predictive control (MPC) of constrained, linear systems. The framework pres... hiện toàn bộ
#Predictive models #Constraint optimization #Predictive control #Linear systems #Design optimization #Functional programming #Strain control #Control systems #Design engineering #Cost function
Multiobjective design using various control techniques
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G.P. Liu, J.F. Whidborne, G.R. Duan
This paper discusses three different multiobjective control schemes: multiobjective PID control, multiobjective critical control and multiobjective eigenstructure assignment. The multiobjective PID control considers a set of frequency-domain performance requirements, such as gain margin, phase margin, crossover frequency and steady-state error. The multiobjective critical control addresses the rob... hiện toàn bộ
#Control systems #Three-term control #Robust control #Robustness #Performance gain #Steady-state #Error correction #Uncertainty #Frequency domain analysis #Eigenvalues and eigenfunctions
An optimisation algorithm for designing fixed-structure controllers using the QFT method
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R. Nandakumar, G.D. Halikias, A.C. Zolotas
We propose a simple optimisation algorithm for designing fixed-structure controllers for highly-uncertain plants. The method can be used to automate the loop-shaping step of the quantitative feedback theory (QFT) design procedure and guarantees robust stability and performance to the feedback loop for all parameters in the plant's uncertainty set. To avoid over-designing the system, the algorithm ... hiện toàn bộ
#Design optimization #Algorithm design and analysis #Uncertainty #Frequency #Feedback #Robustness #Robust control #Robust stability #Design methodology #Automatic control
Neural motion and evolutionary decision in robotic competition applied for molecular machine system design
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Summary form only given. The author presents a new approach within advanced graphics simulations for the problem of nano-assembly automation and its application for nanomedicine. The problem under study concentrates its main focus on the design of autonomous nanorobots for assembly manipulation and the use of evolutionary competitive agents as a suitable way to warranty the robustness of such prop... hiện toàn bộ
#Robotics and automation #Graphics #Robotic assembly #Warranties #Robustness #Neural networks #Robot motion #Sensor systems #Real time systems #Visualization
Multiobjective design for an integrated flight control system: a combination with model reduction approach
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H.H.T. Liu
Modem aircraft include a variety of automatic control systems that aid the flight in navigation, flight management, and augmenting the stability characteristics of the airplane. Typical control systems development involves multiple requirements or objectives. On the other hand, the increasing level of complexity and sophistication of aircraft systems leads to a hierarchical architecture that the o... hiện toàn bộ
#Aerospace control #Reduced order systems #Control systems #Automatic control #Aircraft propulsion #Aircraft navigation #Centralized control #Testing #Modems #Stability