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Adaptive sliding mode control of a hypersonic flight vehicle

dc.contributor.authorXu, H.en
dc.contributor.authorLeung, P.en
dc.contributor.authorMirmirani, M.en
dc.contributor.authorBoussalis, Helen R.en
dc.contributor.authorIoannou, Petros A.en
dc.creatorXu, H.en
dc.creatorLeung, P.en
dc.creatorMirmirani, M.en
dc.creatorBoussalis, Helen R.en
dc.creatorIoannou, Petros A.en
dc.date.accessioned2019-12-02T10:38:56Z
dc.date.available2019-12-02T10:38:56Z
dc.date.issued2001
dc.identifier.urihttp://gnosis.library.ucy.ac.cy/handle/7/57795
dc.description.abstractA Multi Input Multi Output (MIMO) adaptive sliding controller is designed and analyzed for the longitudinal dynamics of a generic hypersonic air vehicle. This vehicle model is highly nonlinear, multivariable, unstable and includes 6 uncertainty parameters. Simulation studies were conducted for trimmed cruise conditions of 110,000 ft and Mach 15 where the responses of the vehicle to a step change in altitude and airspeed were evaluated. The commands were 100ft/s step-velocity and 2000ft step-altitude. The controller is evaluated for robustness with respect to parameter uncertainties using simulations. These simulation studies demonstrate that the proposed controller meets the performance requirements with relatively low amplitude control inputs despite parameter uncertainties.en
dc.sourceAdvances in the Astronautical Sciencesen
dc.sourceProceedings of the AAS/AIAA Space Flight Mechanics Meetingen
dc.source.urihttps://www.scopus.com/inward/record.uri?eid=2-s2.0-0035734824&partnerID=40&md5=330e3ff1619abdc16ddb73421d257ef7
dc.subjectComputer simulationen
dc.subjectRobustness (control systems)en
dc.subjectUncertain systemsen
dc.subjectNonlinear control systemsen
dc.subjectControl system analysisen
dc.subjectAdaptive control systemsen
dc.subjectFlight dynamicsen
dc.subjectHypersonic aerodynamicsen
dc.subjectMulti input multi outputen
dc.subjectAdaptive algorithmsen
dc.subjectAdaptive sliding mode controlen
dc.subjectHypersonic flight vehicleen
dc.subjectSliding mode controlen
dc.titleAdaptive sliding mode control of a hypersonic flight vehicleen
dc.typeinfo:eu-repo/semantics/conferenceObject
dc.description.volume108 IIen
dc.description.startingpage1947
dc.description.endingpage1961
dc.author.facultyΣχολή Θετικών και Εφαρμοσμένων Επιστημών / Faculty of Pure and Applied Sciences
dc.author.departmentΤμήμα Μαθηματικών και Στατιστικής / Department of Mathematics and Statistics
dc.type.uhtypeConference Objecten
dc.description.notes<p>Conference code: 59111en
dc.description.notesCited By :3</p>en
dc.contributor.orcidIoannou, Petros A. [0000-0001-6981-0704]
dc.gnosis.orcid0000-0001-6981-0704


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