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contributor authorS. N. Singh
contributor authorAntônio A. R. Coelho
date accessioned2017-05-08T23:17:25Z
date available2017-05-08T23:17:25Z
date copyrightSeptember, 1984
date issued1984
identifier issn0022-0434
identifier otherJDSMAA-26083#203_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/98215
description abstractThis paper describes an approach to control of nonzero set points of uncertain linear systems based on the theory of ultimate boundedness. We derive a nonlinear control which guarantees that every system response is ultimately bounded within a certain neighborhood of the desired nonzero set point. Analytical expressions for the bounds on variations in parameters for ultimate boundedness are obtained. These results are applied to control of a VTOL aircraft whose time-varying parameters are uncertain. Unlike previous works, arbitrary and fast variations in aircraft parameters are allowed. It is shown that the nonlinear controller is effective for larger variation in parameters than the reduced linear controller. Digital simulation results show that the aircraft can be precisely maneuvered in spite of uncertain parameter variations.
publisherThe American Society of Mechanical Engineers (ASME)
titleNonlinear Control of Mismatched Uncertain Linear Systems and Application to Control of Aircraft
typeJournal Paper
journal volume106
journal issue3
journal titleJournal of Dynamic Systems, Measurement, and Control
identifier doi10.1115/1.3149673
journal fristpage203
journal lastpage210
identifier eissn1528-9028
treeJournal of Dynamic Systems, Measurement, and Control:;1984:;volume( 106 ):;issue: 003
contenttypeFulltext


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