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

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

• iNAT-FSSG-1: FOG Based inertial 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
• iMAR delivers the first dozen of INS for COBRA Counter Battery Radar

• iNAT-RQT-400x: RLG Based Navigation, Surveying & Control System (0.001 °/sqrt(hr); ITAR free)
• iNAT-M-II / -III / -IV: Highly Shock & Vibration hardened Navigation, Surveying & Control System (0.001 °/sqrt(hr); ITAR free)

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 inertial Navigation, Surveying & Control System (1 °/h, 1'000 Hz)
• iNAT-CFM: FOG based GNSS aided IMS of class 5 deg/hr

INS/GNSS Systems in MEMS Technology for Navigation, Control, Stabilization, Surveying and AHRS / VRU / MRU (gyro class 5...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-M300: Small Light Weight high performance MEMS IMU based Navigation, Surveying & Control System (500 Hz)
• iNAT-U200/RLD Ultra Light Weight INS for Navigation, Surveying & Control (500 Hz)
• iNAT-MSLG-5: MEMS Based Navigation, Surveying & Control System (5 °/h, 1'000 Hz)
• iNAT-M200-FLAT Miniature MEMS Based Navigation, Surveying & Control System (500 Hz)

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

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