Transition control using multiple adaptive models and an H-infinity controller design Tập 4 - Trang 2621-2626 vol.4 - 2002
Z. Tian, K.A. Hoo
By transition control, it is meant a type of control method that is employed when the plant transitions from one operating state to another as a result of a set point change. This work proposes and develops an intelligent adaptive multiple model approach that simultaneously adapts the model and an H/sub /spl infin// controller parameters. The method is demonstrated on a non-linear chemical reactor...... hiện toàn bộ
#Programmable control #Adaptive control #H infinity control #Open loop systems #Estimation error #Chemical reactors #Chemical engineering #Chemical products #Globalization #Polymers
Development of a closed-loop testing method for a next-generation terminal area automation system Tập 2 - Trang 1325-1330 vol.2 - 2002
J.E. Robinson, D.R. Isaacson
A next-generation air traffic decision support tool, known as the active final approach spacing tool (aFAST), will generate heading, speed and altitude commands to achieve more precise separation of aircraft in the terminal area. The techniques used to analyze the performance of earlier generation decision support tools are not adequate to analyze the performance of aFAST. The paper summarizes the...... hiện toàn bộ
#Automatic testing #System testing #Automation #Aircraft #Performance analysis #Air traffic control #Feedback loop #Aerospace control #Scheduling algorithm #Trajectory
Disturbance rejection for nonlinear systems Tập 5 - Trang 3484-3489 vol.5 - 2002
Zongxuan Sun, Tsu-Chin Tsao
Tracking or rejection of unknown exogenous signals with known generating dynamics is of major concern in feedback control design. Linear feedback control based on the internal model principle achieves asymptotic performance for linear systems with linear exogenous signal dynamics. This paper presents a control design based on the internal model principle to track or reject nonlinear exogenous sign...... hiện toàn bộ
#Nonlinear systems #Aerodynamics #Linear systems #Feedback control #Sufficient conditions #Control design #Regulators #Nonlinear equations #Partial differential equations #Servomechanisms
Điều khiển phi tuyến thông qua theo dõi quỹ đạo tối ưu hóa Dịch bởi AI Tập 5 - Trang 3980-3985 vol.5 - 2002
E. Nagy
Bài báo này trình bày các phương pháp mới cho thiết kế hệ thống điều khiển theo thời gian rời rạc phi tuyến. Các phương pháp này dựa trên tối ưu hóa và sử dụng hoặc là phương pháp tuyến tính hóa gần đúng hoặc là các phương trình phi tuyến gốc để đạt được giải pháp một cách đồng bộ. Vấn đề tối ưu hóa điều khiển với chân trời hữu hạn được giải quyết qua chuỗi tối ưu hóa hai giai đoạn và lặp. Điều kh...... hiện toàn bộ
#Quỹ đạo
An algebraic approach based on symmetry relations of state space matrices for decoupling the dynamics of a large space structure Tập 2 - Trang 1336-1341 vol.2 - 2002
M. Sigut, L. Acosta, F. Martin, L. Moreno, A. Hamilton
In order to design an effective control policy for the 10 m diameter primary mirror of the Grantecan Telescope, the coupling among the segments that compose the mirror through the structure that supports it must be treated. We present the mathematical demonstration of two important results in order to deal with the mirror dynamics decoupling. Those are: 1) the multiplicity of the eigenvalue corres...... hiện toàn bộ
#State-space methods #Mirrors #Actuators #Telescopes #MIMO #Frequency #Physics #Mathematics #Optical design #Eigenvalues and eigenfunctions
H/sub /spl infin// control and parametric controllers for descriptor systems Tập 6 - Trang 4908-4913 vol.6 - 2002
Zhihua Zhao, Qingling Zhang, Xiaodong Liu
In this paper, we study the existing problem of an H/sub /spl infin// controller for descriptor systems. One necessary and sufficient condition is presented by means of two generalized algebraic Riccati inequalities. Using the method of linear fractional transformation, the controller is parametrized by the admissible solutions to the Riccati inequalities with free parameter Q, a real-rational sta...... hiện toàn bộ
#Control systems #Riccati equations #Sufficient conditions #Linear matrix inequalities #Control theory #Educational institutions #Control system synthesis #Modeling #Constraint theory #Robust control
Control allocation in overactuated aircraft under position and rate limiting Tập 1 - Trang 791-796 vol.1
J.D. Boskovic, R.K. Mehra
Existing approaches to control allocation in overactuated aircraft under control input saturation are conservative. This is due to the fact that the solution to the corresponding constrained optimization problem may not be attainable with a chosen control input weighting matrix. On the other hand, there may exist a weighting matrix for which a solution exists under control input constraints. In th...... hiện toàn bộ
#Aircraft #Aerospace control #Control systems #Computer aided analysis #Weight control #Control design #Aerospace simulation #Vehicles #Equations #Constraint optimization
Distributed parameter thermal controllability-the inverse heat conduction problem in materials processing Tập 6 - Trang 4967-4972 vol.6 - 2002
T. Alaeddine, H. Doumanidis
This article addresses the inverse heat conduction problem encountered in thermal manufacturing processes. An open-loop control strategy is developed for distributed parameter conduction systems, based on Galerkin optimization of an energy index employing Green's functions. The surface heat input distribution necessary to generate a desired dynamic temperature field inside a solid body, is analyti...... hiện toàn bộ
#Thermal conductivity #Distributed control #Temperature control #Materials processing #Open loop systems #Manufacturing processes #Process control #Control systems #Green's function methods #Temperature distribution
Safety of a decentralized scheme for free-flight ATMS using mixed integer linear programming Tập 1 - Trang 742-747 vol.1
L. Pallottino, A. Bicchi, S. Pancanti
In this paper we consider policies for free-flight management of air traffic. We consider instantaneous and bounded heading angle deviation as conflict avoidance maneuvers. The corresponding model, resulting in a mixed integer linear programming (MILP) problem allow to solve both conflict detection and conflict resolution problems. The developed algorithm proved successful in a centralized impleme...... hiện toàn bộ
#Mixed integer linear programming #Aircraft #Aerospace safety #Air safety #Vehicle safety #Traffic control #Decision making #Fuels #Collaboration #Distributed control
Nonlinear adaptive backstepping motion control of linear induction motor Tập 4 - Trang 3099-3104 vol.4 - 2002
Chin-I Huang, Ko-Lo Chen, Hou-Tsan Lee, Li-Chen Fu
In this paper, we propose a nonlinear adaptive controller and an adaptive backstepping controller for linear induction motors (LIMs) to achieve speed/position tracking. A nonlinear transformation is proposed to facilitate controller design. Besides, the unique end effect of the LIM is also considered and is well taken care of in our controller design. Stability analysis based on Lyapunov theory is...... hiện toàn bộ
#Programmable control #Adaptive control #Backstepping #Motion control #Synchronous motors #Induction motors #Circuit testing #Control systems #Gears #Force control