Sistema de guía, navegación y retroalimentación para un misil tierra-aire a través de sistemas híbridos
Objectives and study method: This thesis aims to design and to develop a platform that is capable to guide, control a system orientation as well as the position for a missile. The system designed can be also extrapolated to an unmanned aerial vehicle. The platform designed will help to generate tool...
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| Format: | Tesis |
| Language: | English |
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2016
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| Online Access: | http://eprints.uanl.mx/17636/1/Pedro%20Antonio%20Limo%CC%81n%20Di%CC%81az.pdf |
| _version_ | 1824348971748818944 |
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| author | Limón Díaz, Pedro Antonio |
| author_facet | Limón Díaz, Pedro Antonio |
| author_sort | Limón Díaz, Pedro Antonio |
| collection | Tesis |
| description | Objectives and study method: This thesis aims to design and to develop a platform that is capable to guide, control a system orientation as well as the position for a missile. The system designed can be also extrapolated to an unmanned aerial vehicle. The platform designed will help to generate tools to define the orientation and position of a vehicle by acquiring data from an inertial measurement unit in real time. To confirm the platform operation, a co-simulation technique Hardware-InThe-Loop is used. By using this technique, it is possible to divide the platform into the following modules: 1) Sensor module. This module is composed by an accelerometer, gyroscope, magnetometer, barometer, temperature sensor (that are co-integrated in the same board) and an IR camera. 2) Flight computer module. This module has a distributed system architecture. One side is composed by a commertial development FPGA board for data acquisition, a personal computer for processing and displaying data results. Contributions and conclusions: The developing process is to perform a simulation that, separately, communicates the sensor module block with the flight computer module. Once confirmed the data acquisition and the processes, we will proceed to co-integrate all the algorithms into a main one and test the platform with all the instruments. Additionally, we add a communication module that is co-integrated with a radio frequency transceiver to reinforce a wireless communication. A detailed process to implement the embedded system within the FPGA board is included. The specifications for each element used as the sensor, flight computer and communication modules with a comprehensive description of the system generation are shown. Finally, the results of the test, conclusions and recommendations for future work are addressed. |
| first_indexed | 2025-02-06T03:50:20Z |
| format | Tesis |
| id | eptesis-17636 |
| institution | UANL |
| language | English |
| last_indexed | 2025-02-06T03:50:20Z |
| publishDate | 2016 |
| record_format | eprints |
| spelling | eptesis-176362019-11-21T15:26:03Z http://eprints.uanl.mx/17636/ Sistema de guía, navegación y retroalimentación para un misil tierra-aire a través de sistemas híbridos Limón Díaz, Pedro Antonio TL Vehículo Motor, Aeronáutica, Astronáutica Objectives and study method: This thesis aims to design and to develop a platform that is capable to guide, control a system orientation as well as the position for a missile. The system designed can be also extrapolated to an unmanned aerial vehicle. The platform designed will help to generate tools to define the orientation and position of a vehicle by acquiring data from an inertial measurement unit in real time. To confirm the platform operation, a co-simulation technique Hardware-InThe-Loop is used. By using this technique, it is possible to divide the platform into the following modules: 1) Sensor module. This module is composed by an accelerometer, gyroscope, magnetometer, barometer, temperature sensor (that are co-integrated in the same board) and an IR camera. 2) Flight computer module. This module has a distributed system architecture. One side is composed by a commertial development FPGA board for data acquisition, a personal computer for processing and displaying data results. Contributions and conclusions: The developing process is to perform a simulation that, separately, communicates the sensor module block with the flight computer module. Once confirmed the data acquisition and the processes, we will proceed to co-integrate all the algorithms into a main one and test the platform with all the instruments. Additionally, we add a communication module that is co-integrated with a radio frequency transceiver to reinforce a wireless communication. A detailed process to implement the embedded system within the FPGA board is included. The specifications for each element used as the sensor, flight computer and communication modules with a comprehensive description of the system generation are shown. Finally, the results of the test, conclusions and recommendations for future work are addressed. 2016 Tesis NonPeerReviewed text en cc_by_nc_nd http://eprints.uanl.mx/17636/1/Pedro%20Antonio%20Limo%CC%81n%20Di%CC%81az.pdf http://eprints.uanl.mx/17636/1.haspreviewThumbnailVersion/Pedro%20Antonio%20Limo%CC%81n%20Di%CC%81az.pdf Limón Díaz, Pedro Antonio (2016) Sistema de guía, navegación y retroalimentación para un misil tierra-aire a través de sistemas híbridos. Maestría thesis, Universidad Autónoma de Nuevo León. |
| spellingShingle | TL Vehículo Motor, Aeronáutica, Astronáutica Limón Díaz, Pedro Antonio Sistema de guía, navegación y retroalimentación para un misil tierra-aire a través de sistemas híbridos |
| thumbnail | https://rediab.uanl.mx/themes/sandal5/images/tesis.png |
| title | Sistema de guía, navegación y retroalimentación para un misil tierra-aire a través de sistemas híbridos |
| title_full | Sistema de guía, navegación y retroalimentación para un misil tierra-aire a través de sistemas híbridos |
| title_fullStr | Sistema de guía, navegación y retroalimentación para un misil tierra-aire a través de sistemas híbridos |
| title_full_unstemmed | Sistema de guía, navegación y retroalimentación para un misil tierra-aire a través de sistemas híbridos |
| title_short | Sistema de guía, navegación y retroalimentación para un misil tierra-aire a través de sistemas híbridos |
| title_sort | sistema de guia navegacion y retroalimentacion para un misil tierra aire a traves de sistemas hibridos |
| topic | TL Vehículo Motor, Aeronáutica, Astronáutica |
| url | http://eprints.uanl.mx/17636/1/Pedro%20Antonio%20Limo%CC%81n%20Di%CC%81az.pdf |
| work_keys_str_mv | AT limondiazpedroantonio sistemadeguianavegacionyretroalimentacionparaunmisiltierraaireatravesdesistemashibridos |