Multi-objective optimal longitudinal flight control system design for a large flexible transport aircraft.

dc.contributor.advisorLone, Mudassir M.
dc.contributor.advisorWhidborne, James F.
dc.contributor.authorSong, Sipeng
dc.date.accessioned2023-02-15T09:16:48Z
dc.date.available2023-02-15T09:16:48Z
dc.date.issued2018-05
dc.description.abstractThis thesis presents a multi-objective evolutionary algorithm design of a longitudinal optimal controller for a large exible transport aircraft. The algorithm uses a mixed optimization approach based on a combination of Linear Quadratic Regulator(LQR) control and a Multi-Objective Genetic Algorithm (MOGA) to search over a set of possible weighting function structures and parameter values in order to satisfy a number of conflicting design criteria. The proposed approach offers a number of potential optimal solutions lying on or near the Pareto optimal front of competing objectives. The approach is explained in this thesis and some results are presented.en_UK
dc.description.coursenamePhD in Aerospaceen_UK
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/19184
dc.language.isoenen_UK
dc.rights© Cranfield University, 2015. All rights reserved. No part of this publication may be reproduced without the written permission of the copyright holder.
dc.subjectMulti-objective optimisationen_UK
dc.subjectflexible aircraften_UK
dc.subjectMOGAen_UK
dc.subjectLQRen_UK
dc.subjecthandling qualityen_UK
dc.subjectalgorithm designen_UK
dc.titleMulti-objective optimal longitudinal flight control system design for a large flexible transport aircraft.en_UK
dc.typeThesisen_UK

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