DocumentCode
3636425
Title
Evaluation of a double equipped MEMS IMU based on real flight trial scenarios
Author
M. Becker;U. Bestmann;A. Schwithal;P. Hecker;R. Bott;P. Kohl;S. Knedlik;H. Scheyer;E. v. Hinüber
Author_Institution
Institute of Flight Guidance (IFF), Technische Universitaet Braunschweig, Germany
fYear
2010
Firstpage
202
Lastpage
213
Abstract
The Inertial Measurement Unit (IMU) investigated within the presented work consists of two (optional three) dissimilar sets of MEMS accelerometers and gyros, respectively. Both sets are mounted in one enclosure and thus are subject to the same calibration procedure. Different combinations of these dual sensor sets can be used to exploit the complementary sensor properties, e.g. measurement range, resolution and noise characteristics as well as to benefit from redundancy in airborne applications.
Keywords
Micromechanical devices
Publisher
ieee
Conference_Titel
Position Location and Navigation Symposium (PLANS), 2010 IEEE/ION
ISSN
2153-358X
Print_ISBN
978-1-4244-5036-7
Electronic_ISBN
2153-3598
Type
conf
DOI
10.1109/PLANS.2010.5507129
Filename
5507129
Link To Document