INS, IMS, VRUs and IMUs: Inertial Measurement Systems and Vertical Reference Units for OEM applications INS, IMS, VRUs and IMUs: Inertial Measurement Systems and Vertical Reference Units for OEM applications

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) iMAR contracted to deliver navigation for German Federal Office of Civil Protection and Disaster Assistance
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-1: 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-1: 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
Copyright © 1993 - 2020 iMAR Navigation GmbH. All Rights Reserved.

We use cookies on our website. Some of them are essential for the operation of the site, while others help us to improve this site and the user experience (tracking cookies). You can decide for yourself whether you want to allow cookies or not. Please note that if you reject them, you may not be able to use all the functionalities of the site.

More information Ok Decline