contributor author | Chih-Min Lin | |
contributor author | Chen-Ling Ying | |
date accessioned | 2017-05-08T23:59:05Z | |
date available | 2017-05-08T23:59:05Z | |
date copyright | December, 1999 | |
date issued | 1999 | |
identifier issn | 0022-0434 | |
identifier other | JDSMAA-26260#703_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/121850 | |
description abstract | This paper presents a design algorithm of involving robust decoupled control of uncertain multivariable feedback systems. Two-degree-of-freedom system structure is adopted to handle the quantitative robustness and decoupled performance requirements. Quantitative feedback theory is applied for loop compensator design to achieve quantitative robustness. A decoupled model matching approach is employed for prefilter design to achieve input-output decoupling performance. Thus, the design method of two-degree-of-freedom compensators is proposed to achieve decoupled system control with quantitative robust performance. Since internal stability is satisfied, this design method performs appropriately for any stable or unstable, minimum or non-minimum phase system. The AFTI/F-16 flight control system is considered as the design example to illustrate the design algorithm. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Robust Decoupled System Design of Uncertain Multivariable Feedback Systems | |
type | Journal Paper | |
journal volume | 121 | |
journal issue | 4 | |
journal title | Journal of Dynamic Systems, Measurement, and Control | |
identifier doi | 10.1115/1.2802538 | |
journal fristpage | 703 | |
journal lastpage | 708 | |
identifier eissn | 1528-9028 | |
keywords | Design | |
keywords | Feedback | |
keywords | Robustness | |
keywords | Algorithms | |
keywords | Design methodology | |
keywords | Stability | |
keywords | Control systems AND Flight | |
tree | Journal of Dynamic Systems, Measurement, and Control:;1999:;volume( 121 ):;issue: 004 | |
contenttype | Fulltext | |