Browsing by Author "Hwang, DS"
Now showing 1 - 2 of 2
- Results Per Page
- Sort Options
Item type:Item, A practical design for a multivariable proportional-integral controller in industrial applications(1997-07-01) ;Hwang, DS ;Hsu, PL ;電子工程學系及電子研究所 ;電控工程研究所Department of Electronics Engineering and Institute of ElectronicsThis paper proposes a robust proportional-integral (PI) controller design for multivariable complex processes to achieve both well-decoupled and well-damped output behavior. By reformulating PI-controlled processes in a way similar to the LQG/LTR control design problem; the proposed model matching technique in the first design stage successfully results in the robust PI controller with well-decoupled output behavior and sufficient stability. Moreover, control performance can be further improved to achieve well-damped responses by applying gain modification in a second design stage. Both simulated results using chemical processes and experimental results using a wind tunnel have proven the feasibility of the proposed PI controller design in real applications.Item type:Item, A practical design for a robust fault detection and isolation system(1997-03-01) ;Hwang, DS ;Chang, SK ;Hsu, PL ;電控工程研究所Institute of Electrical and Control EngineeringBased on a development for the unknown input observer (UIO) design, this paper presents a straightforward method of designing a robust fault detection and isolation (FDI) system for uncertain systems with unknown inputs. By exploiting the properties of a nominal model structure, we form a basic sec of residuals which is independent of the unknown input but is dependent on the measurements. Then, with this basic residual set, we append a dynamic weighting matrix to the residuals to increase the design freedom for meeting the required detection and isolation performance. Additionally, a generalized residual generator scheme (GRGS) is proposed to synthesize the parity relations for the isolation of faulty sensors in an uncertain system. The proposed strategy is verified through simulation studies performed on the control of a vertical take-off and landing (VTOL) aircraft in the vertical plane.