Modul inerciální navigační jednotky

English title

Inertial measurement unit module

Type

functional specimen

License

required - licence fee

Authors

Šimek Václav, Ing. (DCSY FIT BUT)
Růžička Richard, doc. Ing., Ph.D., MBA (DCSY FIT BUT)
Chudý Peter, doc. Ing., Ph.D. MBA (DCGM FIT BUT)

Keywords

prototyping, avionics, microcontroller, development platform, modular architecture, CAN bus, inertial navigation unit

Description

An inertial measurement unit module with USB and CAN interface. The output from the module features quantities defining the rigid body attitude, rate and accelerations in principal axes and an output from an integrated magnetometer.

Location

Aeroworks Lab (room L209), Faculty of Information Technology, Brno University of Technology, Bozetechova 2, 612 66 Brno

http://www.fit.vutbr.cz/research/prod/index.php.en?id=246

Files

Projects

Smart Autopilot (TA01010678)

Research groups

Security-aware research in information technology (DC1-7-VZ)

Departments

Department of Computer Graphics and Multimedia FIT BUT (DCGM FIT BUT)
Department of Computer Systems FIT BUT (DCSY FIT BUT)