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)

iMAR at Red Bull Air Race with iNAT-M200/SLN (Ascot / Lausitz / Indy 2016)
iNAT-M200 Small Light Weight MEMS Based Navigation, Surveying & Control System (500 Hz) iNAT-4C/SLx: Multi-Redundant MEMS Based Navigation, Surveying & Control System (500 Hz) iNAT-M200-FLAT Miniature MEMS Based Navigation, Surveying & Control System (500 Hz) iSWACO-M200: Navigation & Vehicle Controller for Swarm Control (automated and autonomous driving / flying / saling / diving) iVRU-CB-M: Inertial Measurement System with integrated Strapdown Data Fusion with Odometer Interface and integrated L1 GPS

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

iNAT-FSLG-01: FOG Based Navigation, Surveying & Control System (0.1 °/h, 1'000 Hz) iNAT-FSSG: FOG Based Navigation, Surveying & Control System (1 °/h, 1'000 Hz)

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)

Airbus Helicopters uses iNAT-RQT for Aircraft Testing & Certification SBB uses iNAT-RQT on MEWA12 to survey Gotthard Base Tunnel
iNAT-RQT-400x: RLG Based Navigation, Surveying & Control System ( 0.004 °/h; ITAR free) iNAT-RQH-400x: RLG Based Navigation, Surveying & Control Systems (0.001 °/sqrt(hr), 0.1...0.8 nm/h) iNAV-RQH: Inertial Gyro Navigation System (ring laser gyro based), 0.001 deg/sqrt(hr)

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

iMAR wins Airbus' "SkyTrack" programme
iNAT-FSLG-01: FOG Based Navigation, Surveying & Control System (0.1 °/h, 1'000 Hz) iNAT-FSSG: FOG Based Navigation, Surveying & Control System (1 °/h, 1'000 Hz) iNAT-CFM: FOG based GNSS aided IMS of class 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

iIMU-FSAS-HP: Class 0.1 deg/hr Inertial Measurement System (Gyro + Accel + Odometer) iIMU-FSAS-NG: Class 1 deg/hr IMS (Gyro + Accel + Odometer)

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

iIMU-FSAS-NG: Class 1 deg/hr IMS (Gyro + Accel + Odometer) iIMU-FSAS: Class 1 deg/hr Inertial Measurement System [not for new designs]

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

iIMU-FSAQ: Inertial Measurement System (Gyro + Accelerometer)

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

iFOG-IMU-1: Inertial Measurement Unit, class 1 deg/hr, small size and FOG based

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

iTNAV: Torpedo Navigation System

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

iNAT-CFM: FOG based GNSS aided IMS of class 5 deg/hr

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

iNAT-CFM: FOG based GNSS aided IMS of class 5 deg/hr

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

iNAT-CFM: FOG based GNSS aided IMS of class 5 deg/hr
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