Integration architecture design for implementation of a vector magnetometer on board of unmanned vehicle

Author

Vaispacher, T. ; Breda, R. ; Andoga, R.

Author_Institution

Dept. of Avionics, Tech. Univ. in Kosice, Kosice, Slovakia

fYear

2014

fDate

19-21 Nov. 2014

Firstpage

483

Lastpage

489

Abstract

Content of this contribution is proposal of Inertial Measurement Unit (IMU) for unmanned aerial vehicle. Verification of the real proposal is based on the creation of the integration algorithm utilizing magnetometer data, which outputs are values of speed, distance and attitude angles. Sensor units for proposed measurement unit are chosen considering the criteria, which are described. For this proposal and measurement is used accelerometer ADXL335, gyroscope L3G462A and magnetometer HMC5983. The contribution consist the overview of the chosen mathematical approaches and summary of the results in graphical form. The verification of proposed algorithm is in range of this contribution made on the proposed IMU unit on board of the unmanned aerial vehicle (UAV).

Keywords

accelerometers; autonomous aerial vehicles; gyroscopes; inertial systems; magnetometers; sensor fusion; accelerometer ADXL335; gyroscope L3G462A; inertial measurement unit; integration architecture design; magnetometer HMC5983; unmanned aerial vehicle; vector magnetometer; Acceleration; Accelerometers; Algorithm design and analysis; Equations; Magnetometers; Mathematical model; Proposals;

fLanguage

English

Publisher

ieee

Conference_Titel

Computational Intelligence and Informatics (CINTI), 2014 IEEE 15th International Symposium on

Conference_Location

Budapest

Type

conf

DOI

10.1109/CINTI.2014.7028724

Filename

7028724