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LKF-FS106-A01 FOG Combined INS High Precision Modular Design Inertial Navigation System with RTK Differential Support

LKF-FS106-A01 FOG Combined INS High Precision Modular Design Inertial Navigation System with RTK Differential Support

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Ürün detayları
cayro aralığı:
±500°/s
cayro önyargısı:
≤1 °/s
ivmeölçer aralığı:
±30g
Birleşik Yön Doğruluğu:
0,5° (1σ, Gerçek Zamanlı)
Güç Tüketimi:
≤10w
Boyutlar:
65×70×63mm
Ödeme ve Nakliye Şartları
Ürün Tanımı
LKF-FS106-A01 FOG Combined INS
Product Introduction

FS106-A01 FOG Combined INS is a reliable, cost-effective navigation unit with an integrated receiver, suited for navigation, control and measurement on aircraft, unmanned ground vehicles, unmanned vessels and UAVs.

Built on a modular design, it adopts high-precision silicon optical gyros and MEMS accelerometers. Its multi-sensor fusion filter processes INS and GPS data to model, estimate and compensate inertial errors, delivering accurate combined navigation outputs of attitude, velocity and position.
It offers dedicated modes for airborne, vehicle and shipborne platforms, with vehicle constraint algorithms for long-term high-precision positioning. Customizable software functions including transfer alignment, integrated navigation, pure inertial calculation and attitude-heading reference fully meet varied user demands.
Product Features
  • Domestic Components, High Performance, Modular
  • Supports GNSS Full Frequency Points, High Positioning and Heading Accuracy in Complex Environments
  • Steady-State Operation 10W Power Consumption
  • -40℃ to +70℃ Full Temperature Calibration Compensation
  • Harsh Mechanical Environment Resistance
  • Vibration and Shock Resistance, EMI Resistance
  • Features software online upgrade capability and installation error compensation
  • Self-correction algorithm maintains horizontal attitude accuracy without GNSS
  • Supports RTK Differential
  • Zero Velocity Update and Vehicle Constraint Algorithms Improve Autonomous Accuracy
Application Fields
  • Mobile Surveying Positioning
  • Unmanned Vehicle, Unmanned Ship/Boat
  • Surveying
  • Stabilized Platform
  • Underwater Vehicle
  • SATCOM on the Move
  • Intelligent Driving
  • Missile-Borne Control
  • Intelligent Mining and North Seeking
Technical Specifications
FS106-A01 FOG Combined INS Performance Parameters
Fiber Optic Gyro
Range (°/s) ±500
Bias (°/h) ≤1
Bias Stability (°/h, 10s) ≤0.5
Bias Instability (°/h, Allan, Typ) ≤0.05
Bias Repeatability (°/h, 6 Power Cycles) ≤0.5
Angle Random Walk (°/√h) ≤0.05
Scale Factor Nonlinearity (ppm) ≤200
Cross Coupling (rad) ≤0.001
Bandwidth (Hz) ≥200
FM Accelerometer
Range (g) ±30
Full Temperature Bias (mg, 3σ) ≤0.5
(μg, 10s Smooth) ≤10
Bias Instability (μg, allan, typ) ≤3
Bias Repeatability (ug) ≤10
Velocity Random Walk (m/s/√h) ≤0.01
Scale Factor Nonlinearity (ppm, ±1g) ≤100
Cross Coupling (rad) ≤0.001
Bandwidth (Hz) ≥200Hz
Combined Navigation Accuracy
Combined Heading Accuracy (°, 1σ, Real-Time) 0.5
Combined Horizontal Attitude (°, 1σ, Real-Time) 0.06
Combined Heading Accuracy (°, Post-Processing) 0.06
Combined Horizontal Attitude (°, Post-Processing) 0.01
Combined Horizontal Position (m, 1σ) 3 (Single-Point), 0.02+1ppm(RTK)
Combined Vertical Position (m, 1σ) 5 (Single-Point), 0.03+1ppm (RTK)
Combined Horizontal Velocity (m/s, 1σ) 0.1
Combined Vertical Velocity (m/s, 1σ) 0.15
Satellite Receiver (Built-in)
Timing Accuracy 20ns
Cold Start Positioning Time ≤40s
Startup ≤2s
Positioning Data Update Rate 10Hz
Altitude 10000m
Satellite Mode GPS: L1/L2/L5; BeiDou: B1/B2/B3; GLONASS: L1/L2
Electrical/Mechanical Interface
Power (V) 12~36VDC(Recommended 24V)
Steady-State Power(W) ≤10W
Start Time (s) 3
Communication Interface RS-422
Update Rate (Hz, max) 1000(IMU), 200(INS)
Dimensions (mm×mm×mm) 65×70×63
Weight (g) ≤500
Operating Environment
Operating Temperature -40~70
Storage Temperature -55~85
Vibration 20~2000HZ, 6.06
Shock 100/1ms

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