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QINGDAO NAVI OPTICS TECHNOLOGY CO.,LTD

City: qingdao

Country/Region:china

Tel:86-532-68977475

Contact Person:
Mr.Ming Ming View Contact Details

51 - 60 of 155 Selling leads

Small Size TDF37IMU0 Fiber Optic Inertial Unit with Low Power Consumption and High Accuracy for Dynamic Measurement

Small Size TDF37IMU0 Fiber Optic Inertial Unit Low Power Consumption Overview Fiber optic inertial units have the advantages of small size, light ... 2026-02-12 20:49:52

High Reliability Universal Marine Fiber Optic Inertial Navigation System for USVs and UUVs

High Reliability Model TDF71A Universal Marine Fiber Optic Inertial Navigation System Introduction This all-purpose marine laser inertial navigation ... 2026-02-12 20:49:52

TDL65A Vehicle Mounted Optical Gyro Positioning Equipment with Angular Rate ≥±400°/sec, Bias Repeatability ≤0.006°/h and Weight ＜6kg

Land Force Navigation TDL65A Vehicle-mounted Optical Gyro Positioning And Orientation Equipment 1 Introduction The vehicle-mounted optical gyro ... 2026-02-12 20:49:52

Aviation Navigation TDF46A Airborne Optical Gyro Inertial Navigation System with ≤0.008°/hr Bias Repeatability, ＞20000 hours MTBF, and ≤20μg Months Bias Repeatability

Aviation Navigation TDF46A Airborne Optical Gyro Inertial Navigation 1 Introduction The airborne optical gyro inertial navigation system employs fiber... 2026-02-12 20:49:51

TDL45C Airborne Optical Gyro Inertial Navigation System with ≤20μg Bias Repeatability, ＞15000 hours MTBF, and ≤15min Alignment Time

Aviation Navigation TDL45C Airborne Optical Gyro Inertial Navigation 1 Introduction The airborne optical gyro inertial navigation system (INS) ... 2026-02-12 20:49:51

TDF71A Airborne Optical Gyro Inertial Navigation System with ≤20μg Bias Repeatability, ＞20000 hours MTBF, and ≤0.005°/√hr Random Walk

Aviation Navigation TDF71A Airborne Optical Gyro Inertial Navigation 1 Introduction The airborne optical gyro inertial navigation system (INS) employs ... 2026-02-12 20:49:51

TDF61A Airborne Optical Gyro Inertial Navigation System with ≤50μg Bias Repeatability, ＞20000 Hours MTBF, and ≤0.01°/√hr Random Walk for Aviation Navigation

Aviation Navigation TDF61A Airborne Optical Gyro Inertial Navigation 1 Introduction The airborne optical gyro inertial navigation system (INS) employs ... 2026-02-12 20:49:51