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Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation

Hangzhou Maixinminwei Technology Co., Ltd.
  • Audited Supplier
  • 3 yrs

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Product Highlights

  • No Moving Parts: Solid-state fiber optic design offers high reliability and long service life.
  • CE Certified: Product meets CE certification standards for safety and quality assurance.
  • Digital Output Signal: Provides digital output for seamless integration with navigation and control systems.
  • Multi-Industry Application: Suitable for aerospace, automotive, robotics, and marine navigation systems.
  • Provides stable attitude reference for aerospace, marine navigation, and industrial robotics, reducing cumulative error in long-duration missions.
  • Ensures industrial robots and military vehicles operate reliably in extreme environments like mining and outdoor defense systems.
  • 4kHz/20kHz raw gyro data and 200Hz compensated data meet dynamic response needs with 921600bps RS-422 interface.
  • 820 50g compact structure and factory calibration replace bulky traditional FOGs (e.g., ADIS/SBG) with lower SWaP.
  • Enhances robot motion control and marine navigation precision, reducing errors in industrial metrology and shipborne systems.
  • Simplifies integration for automotive OEMs and aerospace contractors needing uniform performance in mass production.

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Product Images of Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation

Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation pictures & photos
Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation pictures & photos
Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation pictures & photos
Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation pictures & photos
Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
  • Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
  • Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
    Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
  • Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
    Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
  • Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
    Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
  • Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
    Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation

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Product Description

Specification
Parameters
Unit
Requirement
Gyroscope


Zero bias stability (1σ)
°/h
≤0.2
Zero bias repeatability (1σ)
°/h
≤0.2
Random walk coefficient
°/ h1/2
≤0.04
Scale factor nonlinearity
ppm
≤100
Scale factor asymmetry
ppm
≤100
Scale factor repeatability
ppm
≤50
Measuring range
°/s
-300~+300
Bandwidth
Hz
≥300
Resolving power
°/h
≤0.1
Threshold
°/h
≤0.1
Accelerometer
Zero bias stability
g
≤5*10-4
Bandwidth
Hz
≥300
Measuring range
g
-10 ~ +10
Other parameters
Weight
g
820±50
Working temperature
℃
-55 ~ +70
Storage temperature
℃
-55 ~ +70
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Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
Company Profile
Micro Magic Company
Our inertial sensors are known for their high precision, long life and reliability, and are widely used in a variety of industries such as aerospace, automobiles, robotics, and consumer electronics. Strict production and factory inspection processes ensure that each sensor can meet the high requirements of the industry. We provide customized solutions to meet customer-specific needs and help technological innovation in various industries.
Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
Product Introduction
Fiber Optic Gyroscope Inertial Measurement Unit:UF100A
UF100A fiber optic inertial group is a middle precision and small size IMU as Figure 1 shown. It is used to detect the angular velocity and linear acceleration of the carrier's motion, providing information for the carrier's attitude and navigation control. It has the advantages of small size, light weight, no moving parts, high reliability, and long service life. It can be widely used in aviation, aerospace, ships, weapons, coal mine measurement, automotive electronics and other fields.
imensions & Definitions
Fiber Optic Gyroscope Fog Imu Inertial Navigation System - Ins for Aircraft Navigation
FAQ
Q1:What type of IMU is the UF100A?
A:The UF100A is a middle precision fiber optic gyroscope (FOG)-based IMU, integrating fiber optic gyroscopes and MEMS accelerometers to provide angular velocity and linear acceleration data for navigation and attitude control

Q2: What is the precision of the gyroscope?
A:  The UF100A gyroscope has zero bias stability ≤0.2 °/h (1σ), repeatability ≤0.2 °/h, and random walk ≤0.04 °/√h
Q3: What is the accelerometer performance?
A: The accelerometer has zero bias stability ≤5×10-4 g, measuring range ±10 g, and bandwidth ≥300 Hz.

About the Supplier

Hangzhou Maixinminwei Technology Co., Ltd.
Hangzhou Maixinminwei Technology Co., Ltd.
Hangzhou Maixinminwei Technology Co., Ltd.
Hangzhou Maixinminwei Technology Co., Ltd.
Hangzhou Maixinminwei Technology Co., Ltd.
Hangzhou Maixinminwei Technology Co., Ltd.
Hangzhou Maixinminwei Technology Co., Ltd.
Hangzhou Maixinminwei Technology Co., Ltd.

About Our Factory & Business Background

Address
Room 215, 2nd Floor, Building 7, No. 1180, Bin'an Road, Changhe Sub-district, Binjiang District, Hangzhou City, Zhejiang Province
Average Lead Time
Peak Season Lead Time: within 15 workdays
Off Season Lead Time: within 15 workdays

Our Production Capability & Technical Expertise

Main Products
Fog, Mems Imu, Inclinometer, Quartz Accelerometer, Mems Accelerometer, Mems Gyroscope, Fog Based Imu, Mems Ahrs, Mems Ins, Electronic Compass

Our Industry Experience & Global Business Record

Main Markets
Southeast Asia, Mid East, Western Europe

FAQ

What type of IMU is the UF100A?
The UF100A is a middle precision fiber optic gyroscope (FOG)-based IMU, integrating fiber optic gyroscopes and MEMS accelerometers to provide angular velocity and linear acceleration data for navigation and attitude control
Do I need secondary calibration after delivery?
Eliminates integration delays for automotive OEMS and marine contractors needing rapid deployment.
How does FOG differ from MEMS?
UF100A uses FOG technology, delivering 0.2/h zero-bias vs. MEMS (typically 10/h), with 300Hz bandwidth.
Whats the GNSS outage navigation duration?
Marine surveyors rely on this for 10+ minute GNSS blockages in coastal environments.
Are outputs compatible with existing systems?
RS-422 (J30J-21ZKN-J P5) supports 921600bps, 4/20kHz/200Hz, matching industrial control protocols.
Can it be customized for special interfaces?
Optional interface (J30J-21ZKN-J P5) and data format adjustments (200Hz/4kHz/20kHz) available.
Does it maintain accuracy in high-vibration?
Military vehicles and mining machinery operate reliably with shock/vibration, reducing maintenance costs.
Whats the temperature drift range?
Military defense systems and outdoor industrial robots maintain accuracy in Arctic and desert conditions.
Is batch consistency guaranteed?
Aerospace contractors use it for mass-produced drones (excluded) and missile guidance systems requiring uniform performance.
Does it support RTK/INS fusion?
200Hz compensated data (meters/second, ) enables INS/GNSS/RTK fusion with 4kHz raw data for redundancy.

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