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UF200-N High Performance FOG + MEMS Accl Combined IMU Module

UF200-N High Performance FOG + MEMS Accl Combined IMU Module

The UF200-N fiber optic inertial measurement unit is a highly reliable and cost-effective navigation system, widely applicable to navigation, control, and measurement fields represented by aircraft, unmanned vehicles, unmanned ships, and drones.

The inertial measurement unit inherits the modular design philosophy of similar products and employs high-precision silicon optical gyroscopes and high-precision MEMS accelerometers. In addition to its application as an inertial measurement unit, it can also be configured with different software functions according to user needs. Considering the characteristics of some inertial navigation industry applications, it can perform transfer alignment, integrated navigation, pure inertial navigation solution, attitude and heading reference, etc., thereby maximizing the satisfaction of different user needs.

  • Part No, :

    UF200NN
  • Order(MOQ) :

    1
New Products
  • Description

Product Series and Parameters

Parameters UF200-N
Fiber Optic Gyroscope
Measuring range (°/s) ±500 
Zero bias (°/h) 1
Zero-bias stability (°/h, 10s) 0.5
Zero bias repeatability (°/h, 6 power-on tests) 0.5
Random walk in angle (°/√h) 0.02
Scale nonlinearity (ppm) 200
Scale asymmetry (ppm) 200
Scale repeatability (ppm) 200
Cross-coupling (rad) ≤0.001
Bandwidth (Hz) ≥200
MEMS Accelerometer
Measuring range (g) ±30
Zero position (mg) ≤1
Zero bias stability (ug, 10s smoothing) 30
Zero bias repeatability (ug) 30
Speed random walk (m/s/√h) 0.015
Scale factor nonlinearity (mg, ppm) 5
Cross-coupling (rad) 0.001
Bandwidth (Hz) ≥200
Electrical/mechanical interface
Input voltage 5V DC
Power consumption ≤10W
Size 88.9mm×89.55mm
Weight ≤0.5kg
Operating environment
Operating temperature (℃) -40~+70
Storage temperature (℃) -55~+85
Vibration (g/Hz) 6/20~2000
Impact (g) 100g@11ms
Reliability
MTBF/MTTR(h) 10000/0.5
Maintenance BIT 95%

Production process


Product dimension

 

UF300


Application Scenarios

FOG Inertial Measurement Unit application
The FOG (Fiber Optic Gyro) high-precision IMU is suitable for high-end navigation and control scenarios such as UAV/VTOL flight control and guidance, vehicle/ship attitude & heading reference and integrated navigation, antenna/sensor stabilization platforms, and survey-grade mobile mapping (LiDAR/INS)—delivering ultra-low drift, high bias stability, and strong vibration/EMI immunity for demanding environments.
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FAQ

Q1: What type of product is the UF200-N?
A: The UF200-N is a high-performance, low-cost Fiber Optic Inertial Measurement Unit (IMU) that integrates a tri-axis silicon-based fiber optic gyroscope, high-precision MEMS accelerometers, signal processing circuitry, and navigation software. It can be utilized as a standalone IMU or configured to support functions such as transfer alignment, integrated navigation, pure inertial navigation, and attitude and heading reference.
 
Q2: What are the key features of the UF200-N?
A: Key features include:
Core components are domestically sourced, offering high performance, modularity, and lightweight design.
Comprehensive interface options (RS422 / RS232 / PPS, etc.).
Steady-state power consumption of only 10W.
Full-temperature range calibration and compensation (-40°C to +70°C).
High resistance to vibration and shock, and strong immunity to electromagnetic interference (EMI).
Supports online software upgrades and installation error compensation.
 
Q3: What application scenarios is the UF200-N suitable for?
A: Typical applications include:
Mobile mapping and positioning/attitude reference systems.
Autonomous vehicles, unmanned surface vessels (USVs), and unmanned aerial vehicles (UAVs).
Surveying, mapping, and stabilization platforms.
Underwater vehicles and Communication-on-the-Move (COTM) systems.
Intelligent driving, missile guidance, and intelligent mining (North-finding).
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UF200-N High Performance FOG + MEMS Accl Combined IMU Module
The UF200-N fiber optic inertial measurement unit is a highly reliable and cost-effective navigation system, widely applicable to navigation, control, and measurement fields represented by aircraft, unmanned vehicles, unmanned ships, and drones. The inertial measurement unit inherits the modular design philosophy of similar products and employs high-precision silicon optical gyroscopes and high-precision MEMS accelerometers. In addition to its application as an inertial measurement unit, it can also be configured with different software functions according to user needs. Considering the characteristics of some inertial navigation industry applications, it can perform transfer alignment, integrated navigation, pure inertial navigation solution, attitude and heading reference, etc., thereby maximizing the satisfaction of different user needs.
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