Diseño e implementación de una unidad de medición inercial con conexión a bus can para la aviónica en un mini-helicóptero autónomo no tripulado x-cell graphite.

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Bibliographic Details
Title:	Diseño e implementación de una unidad de medición inercial con conexión a bus can para la aviónica en un mini-helicóptero autónomo no tripulado x-cell graphite.
Authors:	Díaz, Jairo Miguel Vergara¹ jvergara@udem.edu.co
Source:	Revista Ingenierías Universidad de Medellin. jul-dic2005, Vol. 4 Issue 7, p111-124. 14p.
Subjects:	Inertial navigation systems, Computerized instruments, Inertial navigation (Aeronautics), Remotely piloted vehicles, Aeronautical systems engineering
Abstract (English):	This article shows the design and implementation of an inertial measurement unit (IMU) for a mini-helicopter X-CELL Graphite. The application is supported on components COTS (commercial-off-the-shelf) allowing to have the data outputs through a bus CAN. The sensors' operation principles, the form in which the signals of the sensors are processed and the delivery of the measurements of accelerations and angular velocities are well illustrated. Also the importance of this type of measurements in order to obtain the attitude of an aerial vehicle is included. The technology used in the design is based on an implementation of open form for any system that requires it, allowing to have quite high connectivity alternatives for aeronautical applications. [ABSTRACT FROM AUTHOR]
Abstract (Spanish):	Este artículo muestra el diseño y la implementación de una unidad de medición inercial (IMU) basada en componentes COTS (commercial-off-the-shelf) con salida de datos a través de bus CAN para un helicóptero X-CELL Graphite. Se ilustra el principio de funcionamiento de cada sensor, la forma en que la señal de los sensores es procesada y la entrega de las mediciones de aceleraciones y velocidades angulares. También se incluye la importancia de este tipo de mediciones para obtener la actitud de un vehículo aéreo, en este caso, un mini-helicóptero. La tecnología empleada en este diseño está basada en una implementación de forma abierta para cualquier sistema que lo requiera, permitiendo alternativas de conectividad bastante altas para aplicaciones del sector aeronáutico. [ABSTRACT FROM AUTHOR]
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Database:	Engineering Source

Description
Abstract:	This article shows the design and implementation of an inertial measurement unit (IMU) for a mini-helicopter X-CELL Graphite. The application is supported on components COTS (commercial-off-the-shelf) allowing to have the data outputs through a bus CAN. The sensors' operation principles, the form in which the signals of the sensors are processed and the delivery of the measurements of accelerations and angular velocities are well illustrated. Also the importance of this type of measurements in order to obtain the attitude of an aerial vehicle is included. The technology used in the design is based on an implementation of open form for any system that requires it, allowing to have quite high connectivity alternatives for aeronautical applications. [ABSTRACT FROM AUTHOR]
ISSN:	16923324