C Conferentia Proceedings
CON-2016-1589 05. ENGENHARIA AEROESPACIAL

Attitude estimation analysis obtained from MEMs and inertial class gyros using Quaternions and Euler angles approach

Cesar Moura Batagini1; Thiago Neves Cunha1; Euler Gonçalves Barbosa1

1 Instituto de Aeronautica e Espaço - IAE

doi:10.20906/CPS/CON-2016-1589

Resumo

The direction which a vehicle is pointing at can be represented in the Cartesian coordinates system and is also known as vehicle attitude. The attitude parameters depend on angular velocities and the inertial sensor that measures the vehicle's angular velocity is the gyro. Attitude parameters, estimated in Euler angles and quaternions provide these Cartesian coordinates and are going to be discussed in this paper. The accuracy of both estimations is campared. The attitude parameters are provided by two inertial sensors (MEMS-based and velocity sensor gyros) calculated in a real time computer installed in a motion simulating table.

Palavras-chave: Attitude; Quaternions; Euler Angles; MEMS-based gyro

Como citar

Cesar Moura Batagini; Thiago Neves Cunha; Euler Gonçalves Barbosa. “Attitude estimation analysis obtained from MEMs and inertial class gyros using Quaternions and Euler angles approach”. IX Congresso Nacional de Engenharia Mecânica. CONEM2016. 2016. DOI: 10.20906/CPS/CON-2016-1589