Zobrazit minimální záznam

Miniature navigation system for UAS application



dc.contributor.advisorRoháč Jan
dc.contributor.authorGrigoris Panagiotis Mantaos
dc.date.accessioned2022-06-01T09:51:32Z
dc.date.available2022-06-01T09:51:32Z
dc.date.issued2022-05-31
dc.identifierKOS-1198417142605
dc.identifier.urihttp://hdl.handle.net/10467/100897
dc.description.abstractThis 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.cze
dc.description.abstractThis 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.eng
dc.publisherČeské vysoké učení technické v Praze. Vypočetní a informační centrum.cze
dc.publisherCzech Technical University in Prague. Computing and Information Centre.eng
dc.rightsA university thesis is a work protected by the Copyright Act. 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 http://www.mkcr.cz/assets/autorske-pravo/01-3982006.pdf and the citation ethics http://knihovny.cvut.cz/vychova/vskp.htmleng
dc.rightsVysokoškolská 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 http://www.mkcr.cz/assets/autorske-pravo/01-3982006.pdf a citační etikou http://knihovny.cvut.cz/vychova/vskp.htmlcze
dc.subjectUAVcze
dc.subjectIMUcze
dc.subjectINScze
dc.subjectGNSScze
dc.subjectAided Navigationcze
dc.subjectInertial Navigationcze
dc.subjectKalman filtercze
dc.subjectUAVeng
dc.subjectIMUeng
dc.subjectINSeng
dc.subjectGNSSeng
dc.subjectAided Navigationeng
dc.subjectInertial Navigationeng
dc.subjectKalman filtereng
dc.titleMiniaturní navigační systém pro bezpilotní létající prostředkycze
dc.titleMiniature navigation system for UAS applicationeng
dc.typediplomová prácecze
dc.typemaster thesiseng
dc.contributor.refereeVelychko Vitaliy
theses.degree.disciplineAvionikacze
theses.degree.grantorkatedra měřenícze
theses.degree.programmeAerospace Engineeringcze


Soubory tohoto záznamu





Tento záznam se objevuje v následujících kolekcích

Zobrazit minimální záznam