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contributor authorS. Weissenberger
date accessioned2017-05-08T23:00:25Z
date available2017-05-08T23:00:25Z
date copyrightJune, 1976
date issued1976
identifier issn0022-0434
identifier otherJDSMAA-26037#167_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88491
description abstractCommands are found to drive a linear system to optimally track a class of prescribed trajectories, each of which contains a point of discontinuity. The paper focuses on the guidance problem of command generation, to be implemented in a feedforward fashion; the necessary additional control or feedback regulation structure is not studied in detail, but assumed to be provided in applications as a conventional error-feedback regulator. Solutions are found for the infinite-time problem which are optimal with respect to a quadratic performance criterion; suboptimal controls which satisfy a continuity condition are also found. The controls have applications to certain problems in aircraft guidance where command trajectories are piecewise continuous. Several examples are worked out in detail, with comparisons with conventional, nonfeedforward solutions to the problem, and a brief discussion of a simpler, suboptimal solution.
publisherThe American Society of Mechanical Engineers (ASME)
titleOptimal Command Generation for Tracking a Class of Discontinuous Trajectories
typeJournal Paper
journal volume98
journal issue2
journal titleJournal of Dynamic Systems, Measurement, and Control
identifier doi10.1115/1.3427005
journal fristpage167
journal lastpage172
identifier eissn1528-9028
keywordsAircraft
keywordsErrors
keywordsFeedback
keywordsFeedforward control AND Linear systems
treeJournal of Dynamic Systems, Measurement, and Control:;1976:;volume( 098 ):;issue: 002
contenttypeFulltext


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