Development, Modelling and Control of a Multirotor Vehicle

The interest of drones in all forms has exploded in the recent years. The development of multirotor vehicles such as quadcopters and octocopters, has reached a point where they are cheap and versatile enough to start becoming a part of everyday life. It is clear to say that the future applications s...

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Main Author: Mikkelsen, Markus
Format: Others
Language:English
Published: Umeå universitet, Institutionen för tillämpad fysik och elektronik 2015
Subjects:
Online Access:http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-110889
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spelling ndltd-UPSALLA1-oai-DiVA.org-umu-1108892015-11-11T05:08:09ZDevelopment, Modelling and Control of a Multirotor VehicleengMikkelsen, MarkusUmeå universitet, Institutionen för tillämpad fysik och elektronik2015MultirotorOctocopterBlade flappingInduced dragGyroscopic torqueDroneModellingControlCode generationRaspberry PiMatlabSimulinkSimulationsFlight testsThe interest of drones in all forms has exploded in the recent years. The development of multirotor vehicles such as quadcopters and octocopters, has reached a point where they are cheap and versatile enough to start becoming a part of everyday life. It is clear to say that the future applications seem limitless. This thesis goes through the steps of development, modelling and control design of an octocopter system. The developed octocopter builds on a concept of using the mini computer Raspberry Pi together with the code generation functionality of Matlab/Simulink. The mathematical modelling of the octocopter includes the thrust and torques generated by the propellers, added with gyroscopic torque. These are combined with the aerodynamic effects caused by incoming air. The importance of modelling the later mentioned effects has increased with the demand of precise controlled extreme manoeuvres. A full state feedback based hybrid controller scheme is designed against a linearized model, which makes use of the motor dynamics. The controllers show good performance in simulations and are approved for flight tests, which are conducted on two separate occasions. The octocopter makes two successful flights, proving that the concept can be applied on multirotor vehicles. However, there is a miss-match between the mathematical model and the physical octocopter, leaving questions for future work. Student thesisinfo:eu-repo/semantics/bachelorThesistexthttp://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-110889application/pdfinfo:eu-repo/semantics/openAccess
collection NDLTD
language English
format Others
sources NDLTD
topic Multirotor
Octocopter
Blade flapping
Induced drag
Gyroscopic torque
Drone
Modelling
Control
Code generation
Raspberry Pi
Matlab
Simulink
Simulations
Flight tests
spellingShingle Multirotor
Octocopter
Blade flapping
Induced drag
Gyroscopic torque
Drone
Modelling
Control
Code generation
Raspberry Pi
Matlab
Simulink
Simulations
Flight tests
Mikkelsen, Markus
Development, Modelling and Control of a Multirotor Vehicle
description The interest of drones in all forms has exploded in the recent years. The development of multirotor vehicles such as quadcopters and octocopters, has reached a point where they are cheap and versatile enough to start becoming a part of everyday life. It is clear to say that the future applications seem limitless. This thesis goes through the steps of development, modelling and control design of an octocopter system. The developed octocopter builds on a concept of using the mini computer Raspberry Pi together with the code generation functionality of Matlab/Simulink. The mathematical modelling of the octocopter includes the thrust and torques generated by the propellers, added with gyroscopic torque. These are combined with the aerodynamic effects caused by incoming air. The importance of modelling the later mentioned effects has increased with the demand of precise controlled extreme manoeuvres. A full state feedback based hybrid controller scheme is designed against a linearized model, which makes use of the motor dynamics. The controllers show good performance in simulations and are approved for flight tests, which are conducted on two separate occasions. The octocopter makes two successful flights, proving that the concept can be applied on multirotor vehicles. However, there is a miss-match between the mathematical model and the physical octocopter, leaving questions for future work.
author Mikkelsen, Markus
author_facet Mikkelsen, Markus
author_sort Mikkelsen, Markus
title Development, Modelling and Control of a Multirotor Vehicle
title_short Development, Modelling and Control of a Multirotor Vehicle
title_full Development, Modelling and Control of a Multirotor Vehicle
title_fullStr Development, Modelling and Control of a Multirotor Vehicle
title_full_unstemmed Development, Modelling and Control of a Multirotor Vehicle
title_sort development, modelling and control of a multirotor vehicle
publisher Umeå universitet, Institutionen för tillämpad fysik och elektronik
publishDate 2015
url http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-110889
work_keys_str_mv AT mikkelsenmarkus developmentmodellingandcontrolofamultirotorvehicle
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