Miniature navigation system for UAS application

dc.contributor.advisor Roháč, Jan
dc.contributor.author Mantaos, Grigoris Panagiotis
dc.contributor.referee Velychko Vitaliy
dc.date.accessioned 2022-06-01T09:51:32Z
dc.date.available 2022-06-01T09:51:32Z
dc.date.issued 2022-05-31
dc.description.abstract This diploma thesis will outline the design and programming of an Inertial Navigation System, dubbed Mini-INS. The completed system will, like most INS platforms, provide as output the 9-DOF state of a host vehicle in terms of Position, Velocity and Attitude (PVA). Specifically, the implementation will focus on the navigational requirements of Unmanned Aerial Systems (UAS). However, no discrimination shall be made on flight mechanics, meaning that the Mini-INS should be a thorough plug-and-play solution for any aerial or land vehicle, be it a fixed-wing drone, a multi-copter, or a caterpillar tracked robot. In the context of this implementation, the system is designed and manufactured from top to bottom. This includes the hardware design of a schematic, its realization on a Printed Circuit Board (PCB), and its programming so that it may execute the functions of an INS. The primary objective, as the title suggests, is to build a navigation system for use by small unmanned vehicles. As a consequence, the focus of the design will be to minimize the size of the PCB footprint, as well as the board's total power consumption. To achieve this, the board utilizes a combination of MEMS sensors and a low-power ARM microprocessor. cs
dc.description.abstract This diploma thesis will outline the design and programming of an Inertial Navigation System, dubbed Mini-INS. The completed system will, like most INS platforms, provide as output the 9-DOF state of a host vehicle in terms of Position, Velocity and Attitude (PVA). Specifically, the implementation will focus on the navigational requirements of Unmanned Aerial Systems (UAS). However, no discrimination shall be made on flight mechanics, meaning that the Mini-INS should be a thorough plug-and-play solution for any aerial or land vehicle, be it a fixed-wing drone, a multi-copter, or a caterpillar tracked robot. In the context of this implementation, the system is designed and manufactured from top to bottom. This includes the hardware design of a schematic, its realization on a Printed Circuit Board (PCB), and its programming so that it may execute the functions of an INS. The primary objective, as the title suggests, is to build a navigation system for use by small unmanned vehicles. As a consequence, the focus of the design will be to minimize the size of the PCB footprint, as well as the board's total power consumption. To achieve this, the board utilizes a combination of MEMS sensors and a low-power ARM microprocessor. en
dc.identifier KOS-1198417142605
dc.identifier.uri http://hdl.handle.net/10467/100897
dc.publisher České vysoké učení technické v Praze cs
dc.publisher Czech Technical University in Prague en
dc.rights A university thesis is a work protected by the Copyright Act of the Czech Republic. Extracts, copies and transcripts of the thesis are allowed for personal use only and at one`s own expense. The use of thesis should be in compliance with the Copyright Act. en
dc.rights Vysokoškolská závěrečná práce je dílo chráněné autorským zákonem. Je možné pořizovat z něj na své náklady a pro svoji osobní potřebu výpisy, opisy a rozmnoženiny. Jeho využití musí být v souladu s autorským zákonem v platném znění. cs
dc.subject UAV cs
dc.subject IMU cs
dc.subject INS cs
dc.subject GNSS cs
dc.subject Aided Navigation cs
dc.subject Inertial Navigation cs
dc.subject Kalman filter cs
dc.subject UAV en
dc.subject IMU en
dc.subject INS en
dc.subject GNSS en
dc.subject Aided Navigation en
dc.subject Inertial Navigation en
dc.subject Kalman filter en
dc.title Miniaturní navigační systém pro bezpilotní létající prostředky cs
dc.title Miniature navigation system for UAS application en
dc.type master thesis en
dspace.entity.type Publication
relation.isAdvisorOfPublication 909a936c-4c14-463c-88cf-4560debf2b9b
relation.isAdvisorOfPublication.latestForDiscovery 909a936c-4c14-463c-88cf-4560debf2b9b
relation.isAuthorOfPublication fa60a1fd-d6f9-487f-a4d8-b01a85d2eba6
relation.isAuthorOfPublication.latestForDiscovery fa60a1fd-d6f9-487f-a4d8-b01a85d2eba6
theses.degree.discipline Avionika cs
theses.degree.grantor katedra měření cs
theses.degree.programme Aerospace Engineering cs

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