DocumentCode
3628419
Title
The instability measurements for the unmanned aerial platform as a radar carrier
Author
Wojciech Komorniczak;Adam Kawalec;Jerzy Pietrasinski
Author_Institution
Institute Of Radioelectronics, Faculty of Electronics, Military University of Technology, 2 Gen. Kaliskiego Str., 00908 Warsaw, POLAND
fYear
2008
Firstpage
1
Lastpage
4
Abstract
The paper presents the testbed for the UAS instability measurements. The testbed consists of the aerial vehicle of the miniUAV class. The airplane is equipped with the sensor suite built upon several sensing devices: gyroscopes, accelerometers, magnetometers, GPS receiver and pressure sensors. The data from the sensors is combined in the on-board sensor fusion processor and then transmitted to the ground control station. The aerial vehicle that was acting as a carrier platform is a regular UAV being an equipment of one of the European armies.
Keywords
"Process control","Airplanes","Accelerometers","Gyroscopes","Synthetic aperture radar","Testing","Magnetometers"
Publisher
ieee
Conference_Titel
Radar Symposium, 2008 International
ISSN
2155-5745
Print_ISBN
978-83-7207-757-8
Electronic_ISBN
2155-5753
Type
conf
DOI
10.1109/IRS.2008.4585709
Filename
4585709
Link To Document