dc.contributor.advisor |
Savvaris, Al |
|
dc.contributor.author |
Jamil, Ramey |
|
dc.date.accessioned |
2016-10-14T08:19:08Z |
|
dc.date.available |
2016-10-14T08:19:08Z |
|
dc.date.issued |
2012 |
|
dc.identifier.uri |
http://dspace.lib.cranfield.ac.uk/handle/1826/10735 |
|
dc.description.abstract |
Performance and redundancy requirements imposed on state-of-the-art unmmaned
combat aerial vehicles often lead to over-actuated systems with a mix
of conventional and novel moment generators. Consequently, control allocation
schemes have become a crucial part of the flight control architecture and
their design is now a growing problem. This thesis presents a four control
allocation scheme designed to meet multiple objectives and resolve objective
conflicts by finding the ‘Pareto’ optimal solution, namely; Weighted Control
Allocation, Minimax Control Allocation, Canonical Control Allocation and
Classical. This is defined as a solution to the multi-objective optimisation
problem which is non-dominated for all objectives. The scheme is applied to
a six degrees of freedom nonlinear simulation of an aircraft equipped with
conventional control surfaces as well as fluidic thrust vectoring and circulation
control. The results indicate a perfect allocation of the total control
demand onto the actuator suite. |
en_UK |
dc.language.iso |
en |
en_UK |
dc.publisher |
Cranfield University |
en_UK |
dc.rights |
© Cranfield University, 2012. All rights reserved. No part of this publication may be reproduced without the written permission of the copyright holder. |
en_UK |
dc.title |
Multi-objective control allocation |
en_UK |
dc.type |
Thesis or dissertation |
en_UK |
dc.type.qualificationlevel |
Doctoral |
en_UK |
dc.type.qualificationname |
PhD |
en_UK |