Trajectory generation for autonomous unmanned aircraft using inverse dynamics

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dc.contributor.advisor Tsourdos, Antonios
dc.contributor.advisor Cooke, Alastair K.
dc.contributor.author Drury, R. G.
dc.date.accessioned 2011-06-24T14:44:48Z
dc.date.available 2011-06-24T14:44:48Z
dc.date.issued 2010-09
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/5583
dc.description.abstract The problem addressed in this research is the in-flight generation of trajectories for autonomous unmanned aircraft, which requires a method of generating pseudo-optimal trajectories in near-real-time, on-board the aircraft, and without external intervention. The focus of this research is the enhancement of a particular inverse dynamics direct method that is a candidate solution to the problem. This research introduces the following contributions to the method. A quaternion-based inverse dynamics model is introduced that represents all orientations without singularities, permits smooth interpolation of orientations, and generates more accurate controls than the previous Euler-angle model. Algorithmic modifications are introduced that: overcome singularities arising from parameterization and discretization; combine analytic and finite difference expressions to improve the accuracy of controls and constraints; remove roll ill-conditioning when the normal load factor is near zero, and extend the method to handle negative-g orientations. It is also shown in this research that quadratic interpolation improves the accuracy and speed of constraint evaluation. The method is known to lead to a multimodal constrained nonlinear optimization problem. The performance of the method with four nonlinear programming algorithms was investigated: a differential evolution algorithm was found to be capable of over 99% successful convergence, to generate solutions with better optimality than the quasi- Newton and derivative-free algorithms against which it was tested, but to be up to an order of magnitude slower than those algorithms. The effects of the degree and form of polynomial airspeed parameterization on optimization performance were investigated, and results were obtained that quantify the achievable optimality as a function of the parameterization degree. Overall, it was found that the method is a potentially viable method of on-board near- real-time trajectory generation for unmanned aircraft but for this potential to be realized in practice further improvements in computational speed are desirable. Candidate optimization strategies are identified for future research. en_UK
dc.language.iso en en_UK
dc.publisher Cranfield University en_UK
dc.rights © Cranfield University 2010. All rights reserved. No part of this publication may be reproduced without the written permission of the copyright owner. en_UK
dc.subject Autonomy en_UK
dc.subject differential evolution en_UK
dc.subject direct methods en_UK
dc.subject inverse dynamics en_UK
dc.subject near-real-time en_UK
dc.subject negative-g en_UK
dc.subject nonlinear programming en_UK
dc.subject numerical optimization en_UK
dc.subject optimal control en_UK
dc.subject quaternions en_UK
dc.subject trajectory generation en_UK
dc.subject UAV en_UK
dc.subject unmanned aircraft en_UK
dc.title Trajectory generation for autonomous unmanned aircraft using inverse dynamics en_UK
dc.type Thesis or dissertation en_UK
dc.type.qualificationlevel Doctoral en_UK
dc.type.qualificationname PhD en_UK


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