iIMU-CFM-01: FOG/MEMS Based IMU for Surveying, Aviation and ADAHRS Applications
The iIMU-CFM-01 is an IMU consisting of 3 FOG gyros of class 5 deg/hr bias stability and 3 accelerometer axes of class 2 mg, designed according to DO254 and DO160E.
Major features are:
- 0.3 deg/sqrt(hr) / 50 µg/sqrt(Hz); bias stability (AV) 0.2 °/hr, 0.1 mg @ const. temp.
- 1’000 Hz and 200 Hz data rate with calibrated data
- power supply according to DO160E; FPGA firmware and hardware according to DO254, DAL A.
- Applications: Attitude Heading Reference, Surveying, Guidance & Control
- RS485 (UART) interface
- SYNC input for time stamping
- Optional CAN interface
The iIMU-CFM-01 is designed for ruggedized applications on land vehicles, naval vessels, helicopters, fixed wing aircrafts and UAVs. The iIMU-CFM-01 can be operated at an unregulated wide range power supply (10-34 V DC)and is protected against wrong polarity, HIRF, SEU, lightning, and over-voltage up to 80 V. The data output is free running and the data are sent via RS485. Two redundant outputs and power supply inputs are available.
The iIMU-CFM-01 requires no export license.
The iIMU-MM-04 uses MEMS gyro technology and servo accelerometers. It is interface compatible to iIMU-CFM-01.
Further informations:
Datasheet iIMU-CFM-01 (FOG based IMU, 5 deg/hr OTR)
Datasheet iIMU-MM-04 (MEMS based IMU, 15 deg/hr OTR)
