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 :
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