DocumentCode
3567710
Title
Inertial laboratory simulation
Author
Blum, C. ; Braun, B. ; Dambeck, J. ; Kagi, M.
Author_Institution
Inst. of Flight Syst. Dynamics (TUM), Garching, Germany
fYear
2014
Firstpage
1
Lastpage
16
Abstract
In early 2015 an inertial laboratory will be installed at TUM´s Institute of Flight System Dynamics (FSD). In cooperation with ACUTRONIC Switzerland Ltd. an AC3350 three-axis motion simulator will be used to investigate inertial sensor calibration techniques, as well as error influences of the whole laboratory environment. To identify and assess possible influences on the laboratory´s quality a simulation of the whole calibration process, including error models of the laboratory environment, the motion simulator and the unit under test has been created. The article presents an overview of identified error sources in the inertial sensor calibration process. Typical error sources are discussed exemplarily for the future Inertial Laboratory. Finally the influence of these errors on a symmetric six-pose calibration process is illustrated using preliminary simulation results.
Keywords
aerospace simulation; aircraft navigation; calibration; electric sensing devices; inertial navigation; measurement errors; AC3350; error model; error source identification; flight system dynamics; inertial laboratory simulation; inertial sensor calibration technique; laboratory environment; symmetric six pose calibration process; three axis motion simulator; unit under test; Calibration; Damping; Dynamics; Laboratories; Sensors; Soil; Surface waves;
fLanguage
English
Publisher
ieee
Conference_Titel
Inertial Sensors and Systems Symposium (ISS), 2014 DGON
Type
conf
DOI
10.1109/InertialSensors.2014.7049473
Filename
7049473
Link To Document