Assessment of noise of MEMS IMU sensors of different grades for GNSS/IMU navigation

Inertial measurement units (IMUs) are key components of various applications including navigation, robotics, aerospace, and automotive systems. IMU sensor characteristics have a significant impact on the accuracy and reliability of these applications. In particular, noise characteristics and bias st...

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Detalhes bibliográficos
Autores: Suvorkin, Vladimir|||0000-0001-7928-3266, García Fernández, Miquel|||0000-0003-4844-6004, González Casado, Guillermo|||0000-0001-6765-2407, Li, Mowen, Rovira Garcia, Adrià|||0000-0002-7320-5029
Tipo de documento: artigo
Data de publicação:2024
País:España
Recursos:Universitat Politècnica de Catalunya (UPC)
Repositório:UPCommons. Portal del coneixement obert de la UPC
Idioma:inglês
OAI Identifier:oai:upcommons.upc.edu:2117/406506
Acesso em linha:https://hdl.handle.net/2117/406506
https://dx.doi.org/10.3390/s24061953
Access Level:Acceso aberto
Palavra-chave:Artificial satellites in navigation
Microelectromechanical systems
Inertial navigation systems
Galileo satellite navigation system
IMU
MEMS
OADEV
GNSS
Sensor fusion
Loosely coupled
Sistemes microelectromecànics
Sistemes de navegació inercial
Satèl·lits artificials en navegació
Àrees temàtiques de la UPC::Enginyeria electrònica
Descrição
Resumo:Inertial measurement units (IMUs) are key components of various applications including navigation, robotics, aerospace, and automotive systems. IMU sensor characteristics have a significant impact on the accuracy and reliability of these applications. In particular, noise characteristics and bias stability are critical for proper filter settings to perform a combined GNSS/IMU solution. This paper presents an analysis based on the Allan deviation of different IMU sensors that correspond to different grades of micro-electromechanical systems (MEMS)-type IMUs in order to evaluate their accuracy and stability over time. The study covers three IMU sensors of different grades (ascending order): Rokubun Argonaut navigator sensor (InvenSense TDK MPU9250), Samsung Galaxy Note10 phone sensor (STMicroelectronics LSM6DSR), and NovAtel PwrPak7 sensor (Epson EG320N). The noise components of the sensors are computed using overlapped Allan deviation analysis on data collected over the course of a week in a static position. The focus of the analysis is to characterize the random walk noise and bias stability, which are the most critical for combined GNSS/IMU navigation and may differ or may not be listed in manufacturers’ specifications. Noise characteristics are calculated for the studied sensors and examples of their use in loosely coupled GNSS/IMU processing are assessed. This work proposes a structured and reproducible approach for working with sensors for their use in navigation tasks in combination with GNSS, and can be used for sensors of different levels to supplement missing or incorrect sensor manufacturers’ data.