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Navigation Functionalities for an Autonomous UAV Helicopter

Navigation Functionalities for an Autonomous UAV Helicopter

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LINKÖPINGS UNIVERSITET<br />

Språk<br />

L<strong>an</strong>guage<br />

X<br />

Svenska/Swedish<br />

Engelska/English<br />

URL för elektronisk version<br />

Rapporttyp<br />

Report category<br />

Licentiatavh<strong>an</strong>dling<br />

Examensarbete<br />

C-uppsats<br />

D-uppsats<br />

Övrig rapport<br />

Titel<br />

Title<br />

<strong>Navigation</strong> <strong>Functionalities</strong> <strong>for</strong> <strong>an</strong> <strong>Autonomous</strong> <strong>UAV</strong> <strong>Helicopter</strong><br />

Författare<br />

Author<br />

Gi<strong>an</strong>paolo Conte<br />

ISBN<br />

ISRN<br />

Serietitel och serienummer ISSN<br />

Title of series, numbering<br />

Linköping Studies in Science <strong>an</strong>d Technology<br />

Thesis No. 1307<br />

Samm<strong>an</strong>fattning<br />

Abstract<br />

This thesis was written during the WITAS <strong>UAV</strong> Project where one of the goals has been the development of a<br />

software/hardware architecture <strong>for</strong> <strong>an</strong> unm<strong>an</strong>ned autonomous helicopter, in addition to autonomous functionalities<br />

required <strong>for</strong> complex mission scenarios. The algorithms developed here have been tested on <strong>an</strong> unm<strong>an</strong>ned helicopter<br />

plat<strong>for</strong>m developed by Yamaha Motor Comp<strong>an</strong>y called the RMAX.<br />

The character of the thesis is primarily experimental <strong>an</strong>d it should be viewed as developing navigational<br />

functionality to support autonomous flight during complex real-world mission scenarios. This task is<br />

multidisciplinary since it requires competence in aeronautics, computer science <strong>an</strong>d electronics.<br />

The focus of the thesis has been on the development of a control method to enable the helicopter to follow 3D paths.<br />

Additionally, a helicopter simulation tool has been developed in order to test the control system be<strong>for</strong>e flight-tests.<br />

The thesis also presents <strong>an</strong> implementation <strong>an</strong>d experimental evaluation of a sensor fusion technique based on a<br />

Kalm<strong>an</strong> filter applied to a vision based autonomous l<strong>an</strong>ding problem.<br />

Extensive experimental flight-test results are presented.<br />

Nyckelord<br />

Keywords<br />

X<br />

Avdelning, institution<br />

Division, department<br />

Institutionen för datavetenskap<br />

Department of Computer<br />

<strong>an</strong>d In<strong>for</strong>mation Science<br />

978-91-85715-35-0<br />

LiU-Tek-Lic-2007:16<br />

Datum<br />

Date<br />

March 1st, 2007<br />

0280-7971<br />

Unm<strong>an</strong>ned Aerial Vehicle, Control System, Path Following, Path Pl<strong>an</strong>ning, Sensor Fusion, Vision<br />

Based L<strong>an</strong>ding, Kalm<strong>an</strong> Filter, Real-Time.

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