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contributor authorChih-Min Lin
contributor authorChen-Ling Ying
date accessioned2017-05-08T23:59:05Z
date available2017-05-08T23:59:05Z
date copyrightDecember, 1999
date issued1999
identifier issn0022-0434
identifier otherJDSMAA-26260#703_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/121850
description abstractThis 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleRobust Decoupled System Design of Uncertain Multivariable Feedback Systems
typeJournal Paper
journal volume121
journal issue4
journal titleJournal of Dynamic Systems, Measurement, and Control
identifier doi10.1115/1.2802538
journal fristpage703
journal lastpage708
identifier eissn1528-9028
keywordsDesign
keywordsFeedback
keywordsRobustness
keywordsAlgorithms
keywordsDesign methodology
keywordsStability
keywordsControl systems AND Flight
treeJournal of Dynamic Systems, Measurement, and Control:;1999:;volume( 121 ):;issue: 004
contenttypeFulltext


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