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  • INS, IMS, VRUs, MRUs, IMUs: Inertiale Navigations- und Meßsysteme, Vertical Reference Units für OEM Anwendungen

INS, IMS, VRUs, MRUs, IMUs: Inertiale Navigations- und Meßsysteme, Vertical Reference Units für OEM Anwendungen

INS, IMS, VRUs, MRUs, IMUs: Inertiale Navigations- und Meßsysteme, Vertical Reference Units für OEM Anwendungen

INS/GPS Systems in MEMS Technology for Navigation, Control, Stabilization, Surveying and AHRS / VRU / MRU (gyro class 10...100 deg/hr)

IMS of class 0.1 ... 1 deg/hr / 0.01 ... 0.1 deg/sqrt(hr) / 1'000 deg/s / 1 mg / 10 g

INS/GNSS Systems of highest Performance with RLG (Ring Laser Gyro) Technology for Navigation, Stabilization, Guidance and Control (gyro class 0.001...0.05 deg/hr)

INS/GNSS Systems with FOG (Fiber Optical Gyro) Technology for Navigation, Stabilization, Guidance and Control (gyro class 0.05...5 deg/hr)

IMU of class 0.1 deg/h / 0.01 deg/rt-hr , 1.5 mg / 5 g with HDLC / RS422/RS232 (UART) I/F

IMU of class 1 deg/h / 0.15 deg/rt-hr , 1.5 mg / 5 g with HDLC / RS422/RS232 (UART) I/F

IMU of class 1 deg/h / 0.15 deg/rt-hr , 160 µg / 10 g with RS422 (UART) and CAN I/F

IMU of class 1 deg/h / 450 deg/s / 0.1 deg/rt-hr, 1.5 mg / 5 g mit HDLC-I/F / iFOG-IMU-1-A

IMU of class 1 deg/h, 2 mg for Torpedo and AUV applications / iTNAV-06

IMU / System of class 5 deg/h, 2 mg for Aviation Applications / iIMU-CFM

VRU / INS/GSS System in FOG/MEMS Technology of class 5 deg/h, 2 mg for aviation / iNAT-CFM

IMU and AHRS for helicopters and fixed wing aircraft / iIMU-CFM and iNAT-CFM

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