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µIMU (MEMS-based Inertial Measurement Unit)


 
General 
Product Name:µIMU (MEMS-based Inertial Measurement Unit)
Product Description:
Type of application:Air, Land, Marine
Year of initial development:2008
Height [m]:0.06
Width [m]:0.085
Length [m]:0.085
Weight [kg]:0.68
Min. Voltage (AC):
Max. Voltage (AC):
Min. Voltage (DC):4.75
Max. Voltage (DC):5.4
Power consumption [W]:8
Splashproof casting:Y
Water resistant casting:Y
Water resistance [m]:
Mean time between failures [hr]:33000
Type of accelerometer:MEMS
Type of gyro:MEMS
Removable from base plate:N
Moving parts:N
Environmental 
Non-operating shock tolerance [g]:
Operating shock tolerance [g]:40
Min. operating temperature [C]:-55
Max. operating temperature [C]:71
Max. rotation speed [deg/s]:499
Data formats 
NMEA formats:
RTCM:
Other :HDLC
GNSS aided uncertainty 
Heading [deg]:
Pitch [deg]:
Roll [deg]:
Heave: constant part [m]:
Heave: variable part [%]:
Surge/sway [m]:
Increase in position uncertainty w.r.t. stand-alone GPS [m]:
EM log aided uncertainty 
Heading [deg]:
Pitch [deg]:
Roll [deg]:
Heave [m]:
Surge/sway [m]:
Decrease in position accuracy [m/hr]:
Doppler log aided uncertainty 
Heading [deg]:
Pitch [deg]:
Roll [deg]:
Heave [m]:
Surge/sway [m]:
Decrease in position accuracy [m/hr]:
Unaided uncertainty 
Heading [deg]:
Pitch [deg]:
Roll [deg]:
Heave [m]:
Surge/sway [m]:
Decrease in position accuracy [m/hr]:
Inertial Measurement Unit 
Accelerometer bias [µ-g]:10
gyro bias [deg/hr]:6
Calibration procedure:No calibration at customer required.
Software 
Name:
Filtering:
Adaptable filter strength:
Adaptable input signals:
Integrity monitoring of position input:
Integrity monitoring of log input:
Max. number of position input signals:
Max. number of log input signals:
Maximum latency of position input [ms]:
Maximum latency of log input [ms]:
Uncertainty indicators given in output:
Uncertainty of time stamp for output [ms]:
Other specifications 
Export restrictions:µIMU-IC is not export controlled, µIMU-I is classified as dual use, µIMU-M is export controlled
Graphical user interface:
Typical application:photogrammetry systems, navigation systems, attitude and heading reference systems, stabilisation
Distinguishable features:not ITAR-controlled, high performance under harsh environment and over the full temperature range, exceptionel reliability, high MTBF
 


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