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dc.contributor.authorRafi, Melvin
dc.contributor.authorSteck, James E.
dc.contributor.authorWatkins, John Michael
dc.date.accessioned2017-09-07T18:46:43Z
dc.date.available2017-09-07T18:46:43Z
dc.date.issued2017-09
dc.identifier.citationMelvin Rafi, James E. Steck, and John Watkins. "Kalman-Filter-Based Adaptive Control: Flight Testing on General Aviation Aircraft", Journal of Guidance, Control, and Dynamics, Vol. 40, Special Issue on The Kalman Filter and Its Aerospace Applications (2017), pp. 2307-2315en_US
dc.identifier.issn0731-5090
dc.identifier.otherWOS:000408004100015
dc.identifier.urihttp://dx.doi.org/10.2514/1.G002693
dc.identifier.urihttp://hdl.handle.net/10057/14074
dc.descriptionClick on the DOI link to access the article (may not be free).en_US
dc.description.abstractSensor noise and turbulence effects have been prevalent issues in control system design. Although a control system may respond well to “clean” input signals and commands in simulation, this may not be the case when a controller is tasked to perform in a practical environment. A sensor measurement from the plant may be distorted with noise, or turbulence effects may alter controller behavior. Across various engineering disciplines, the notion of engineered resilience has received much attention in efforts to design safer and more reliable systems [1,2] capable of tolerating uncertainties and disturbances.en_US
dc.description.sponsorshipNASA under award number NNXO9AP20A.en_US
dc.language.isoen_USen_US
dc.publisherAmerican Institute of Aeronautics and Astronautics, Inc.en_US
dc.relation.ispartofseriesJournal of Guidance, Control, and Dynamics;v.40:no.9
dc.titleKalman-Filter-Based Adaptive Control: flight testing on general aviation aircraften_US
dc.typeArticleen_US
dc.rights.holderCopyright © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.en_US


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  • AE Research Publications [101]
    Research publications authored by the Department of Aerospace Engineering faculty and graduate students.

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