dc.contributor.advisor |
Whidborne, James F. |
|
dc.contributor.author |
Saban, Deborah |
|
dc.date.accessioned |
2010-05-12T10:15:51Z |
|
dc.date.available |
2010-05-12T10:15:51Z |
|
dc.date.issued |
2010-01 |
|
dc.identifier.uri |
http://hdl.handle.net/1826/4414 |
|
dc.description.abstract |
The aim of this research is to develop realistic models of aerodynamic cross-coupling
e ects that can be incorporated in real-time or near real-time simulations of Unmanned
Aerial Vehicles (UAVs) in close formation flight. These would permit the assessment of
the risks and issues associated with wake vortex evolution and encounter and the analysis
of their consequences on the design of automatic control systems and the development
of safe and reliable operating procedures. A number of wake vortex modelling
techniques that can be used in formation flight simulations are reviewed. A novel Wake
Vortex Model (WVM) is developed, implemented, verified, validated and successfully
integrated within a Matlab/Simulink simulation environment. The code, named ELL
because it is based on Weissinger’s extended lifting line theory, meets the following
requirements: (i) it is generic and can easily be adapted to accomodate any wing planform
and air vehicle configuration; (ii) it is computationally rapid enough to be used in
real-time or near real-time simulations; (iii) and it is sufficiently representative to support
studies of aerodynamic interaction between multiple air vehicles during formation
reconfiguration and air-to-air refuelling simulations. Simulink test scenarios of two
Aerosonde UAVs are developed to test and validate the use of ELL within simulation
models, and the simulation environment is interfaced with visualisation tools in order
to facilitate the evaluation of multiple air vehicle dynamic interaction. |
en_UK |
dc.language.iso |
en |
en_UK |
dc.publisher |
Cranfield University |
en_UK |
dc.rights |
©Cranfield University, 2009. All rights reserved. No part of this publication may be
reproduced without the written permission of the copyright holder. |
en_UK |
dc.title |
Wake Vortex Modelling and Simulation for Air Vehicles in Close Formation Flight |
en_UK |
dc.type |
Thesis or dissertation |
en_UK |
dc.type.qualificationlevel |
Doctoral |
en_UK |
dc.type.qualificationname |
PhD |
en_UK |