dor_id: 45743

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336.#.#.3: Artículo de Investigación

336.#.#.a: Artículo

351.#.#.6: https://jart.icat.unam.mx/index.php/jart

351.#.#.b: Journal of Applied Research and Technology

351.#.#.a: Artículos

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856.4.0.u: https://jart.icat.unam.mx/index.php/jart/article/view/195/192

100.1.#.a: Munguía, R.

524.#.#.a: Munguía, R. (2014). A GPS-aided Inertial Navigation System in Direct Configuration. Journal of Applied Research and Technology; Vol. 12 Núm. 4. Recuperado de https://repositorio.unam.mx/contenidos/45743

245.1.0.a: A GPS-aided Inertial Navigation System in Direct Configuration

502.#.#.c: Universidad Nacional Autónoma de México

561.1.#.a: Instituto de Ciencias Aplicadas y Tecnología, UNAM

264.#.0.c: 2014

264.#.1.c: 2014-08-01

653.#.#.a: Inertial Navigation; Sensor Fusion; State Estimation

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041.#.7.h: eng

520.3.#.a: This work presents a practical method for estimating the full kinematic state of a vehicle, along with sensor errorparameters, through the integration of inertial and GPS measurements. This kind of system for determining attitudeand position of vehicles and craft (either manned or unmanned) is essential for real time, guidance and navigationtasks, as well as for mobile robot applications.The architecture of the system is based in an Extended Kalman filtering approach in direct configuration. In this case,the filter is explicitly derived from the kinematic model, as well as from the models of sensors error. The architecturehas been designed in a manner that it permits to be easily modified, in order to be applied to vehicles with diversedynamical behaviors.The estimated variables and parameters are i) Attitude and bias-compensated rotational speed of the vehicle, ii)Position, velocity and bias-compensated acceleration of the vehicle and iii) bias of gyroscopes and accelerometers.Experimental results with real data show that the proposed method is enough robust for its use along with low-costsensors.

773.1.#.t: Journal of Applied Research and Technology; Vol. 12 Núm. 4

773.1.#.o: https://jart.icat.unam.mx/index.php/jart

022.#.#.a: ISSN electrónico: 2448-6736; ISSN: 1665-6423

310.#.#.a: Bimestral

264.#.1.b: Instituto de Ciencias Aplicadas y Tecnología, UNAM

doi: https://doi.org/10.1016/S1665-6423(14)70096-3

harvesting_date: 2023-11-08 13:10:00.0

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last_modified: 2024-03-19 14:00:00

license_url: https://creativecommons.org/licenses/by-nc-sa/4.0/legalcode.es

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Artículo

A GPS-aided Inertial Navigation System in Direct Configuration

Munguía, R.

Instituto de Ciencias Aplicadas y Tecnología, UNAM, publicado en Journal of Applied Research and Technology, y cosechado de Revistas UNAM

Licencia de uso

Procedencia del contenido

Cita

Munguía, R. (2014). A GPS-aided Inertial Navigation System in Direct Configuration. Journal of Applied Research and Technology; Vol. 12 Núm. 4. Recuperado de https://repositorio.unam.mx/contenidos/45743

Descripción del recurso

Autor(es)
Munguía, R.
Tipo
Artículo de Investigación
Área del conocimiento
Ingenierías
Título
A GPS-aided Inertial Navigation System in Direct Configuration
Fecha
2014-08-01
Resumen
This work presents a practical method for estimating the full kinematic state of a vehicle, along with sensor errorparameters, through the integration of inertial and GPS measurements. This kind of system for determining attitudeand position of vehicles and craft (either manned or unmanned) is essential for real time, guidance and navigationtasks, as well as for mobile robot applications.The architecture of the system is based in an Extended Kalman filtering approach in direct configuration. In this case,the filter is explicitly derived from the kinematic model, as well as from the models of sensors error. The architecturehas been designed in a manner that it permits to be easily modified, in order to be applied to vehicles with diversedynamical behaviors.The estimated variables and parameters are i) Attitude and bias-compensated rotational speed of the vehicle, ii)Position, velocity and bias-compensated acceleration of the vehicle and iii) bias of gyroscopes and accelerometers.Experimental results with real data show that the proposed method is enough robust for its use along with low-costsensors.
Tema
Inertial Navigation; Sensor Fusion; State Estimation
Idioma
eng
ISSN
ISSN electrónico: 2448-6736; ISSN: 1665-6423

Enlaces