gyros quartz aircraft inertial navigation system

Model Number:F70-1

Brand Name:Firepower

F70 low bias fiber gyro low noise optic gyro.pdf NAVIGATION GYRO LOW COST INERTIAL GYRO SENSOR AVIATION GYRO SENSOR The F70 is the interferometric digital close-loop single-axis fiber optic gyro. It is the perfect substitution for traditional mechanical ...

Brand Name:NAVI OPTICS

Model Number:TDF41A

Place of Origin:CHINA

... as its core sensors, employing either a strapdown or dithered (modulated) inertial navigation system architecture. It runs advanced navigation software internally at high speed to provide real-time navigation information. This series of products can

Brand Name:Hfsensing

Model Number:DETA 30 Series

Place of Origin:China

...series, a complete set of industrial-grade micro-inertial navigation systems based on mems and quartz gyroscopes. The feature of this series is the use of redundant sensor technology, which integrates three gyroscopes with a zero bias stability of 2 ° /h

Brand Name:Kacise

Model Number:KsINS-II

Place of Origin:China (Mainland)

KsINS-II fiber optic strapdown inertial navigation system product description: The KsINS-II optical fiber strapdown inertial navigation system is a miniaturized and general-purpose inertial navigation system using high-precision fiber optic gyroscopes and ...

Brand Name:JOHO

Model Number:AINS-20

Place of Origin:CHINA

Aircraft Flight Control Fiber Optic Gyroscope GPS Position And Orientation System Employing high accuracy FOG, Q-flex accelerometers, dual-frequency GPS position & orientation system, barometric altimeter and advanced integration navigation and attitude measurement algorithm, the performance of Attitude and Azimuth Integrated Navigation Fiber Optic Vertical Gyro has been dramatically improved. Combining built-in high accuracy IMU (inertial

Place of Origin:China

Brand Name:Ericco

Model Number:ER-I/G

ER-I/G Smallest Volume Quartz Flexure Accelerometer for Small INS Application ER-I/G is with high performance, small volume and it is used in inertial navigation system of small size. No. Parameter Performance Indicators Unit 02 01 1 Bias ≤5 ≤10 mg 2 Scale...