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FOG Combined INS with High Accuracy and Low Power

FOG Combined INS with High Accuracy and Low Power

≤1°/h Gyro Bias FOG Combined INS

0.5° Combined Heading Accuracy Inertial Navigation System

≤10W Power Consumption Combined Navigation System

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Product Details
Gyro Range:
±500°/s
Gyro Bias:
≤1°/h
Accelerometer Range:
±30g
Combined Heading Accuracy:
0.5° (1σ, Real-Time)
Power Consumption:
≤10W
Dimensions:
65×70×63mm
Highlight:

≤1°/h Gyro Bias FOG Combined INS

,

0.5° Combined Heading Accuracy Inertial Navigation System

,

≤10W Power Consumption Combined Navigation System

Payment & Shipping Terms
Product Description
LKF-FS106-A01 FOG Combined INS
Product Introduction

The FS106-A01 FOG Combined INS is a highly reliable, cost-effective navigation system with built-in receiver, widely applicable to navigation, control, and measurement in aircraft, unmanned vehicles, unmanned ships, and unmanned aerial vehicles.

This combined navigation system inherits the modular design philosophy of similar products, employing high-precision silicon optical gyroscopes and high-precision MEMS accelerometers. Through multi-sensor fusion algorithms, the main INS position and velocity from GPS are fed into the filter, while the INS position, velocity, and attitude also serve as filter inputs. The filter compares the differences between them to establish an error model for estimating INS errors, which are then used to correct the INS results, yielding combined navigation outputs for velocity, position, and attitude.

The inertial navigation system provides different configuration modes to suit various carriers, including airborne, vehicle-mounted, and shipboard applications. Vehicle-mounted mode includes vehicle constraint algorithms. Error estimation and correction enable long-duration high-precision navigation and positioning for carriers.

The FS106-A01 Series Combined Navigation System can be configured differently according to user requirements. Software functions configuration supports transfer alignment, combined navigation, pure INS computation, attitude and heading reference, maximizing satisfaction of diverse user requirements.

Product Features
  • Domestic components, high performance, modular design
  • Supports GNSS full frequency points, high positioning and heading accuracy in complex environments
  • Multiple port options available
  • Steady-state operation with 10W power consumption
  • -40℃ to +70℃ full temperature calibration compensation
  • Harsh mechanical environment resistance
  • Vibration and shock resistance, EMI resistance
  • 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 applications
  • Stabilized platform systems
  • Underwater vehicle navigation
  • SATCOM on the move
  • Intelligent driving systems
  • Missile-borne control
  • Intelligent mining and north seeking
Technical Specifications
Table 1: FS106-A01 FOG Combined INS Performance Parameters

Performance Parameters

Fiber Optic Gyroscope

Range (° /s)

±500

Bias Stability (° /h, 10s)

0.5

Bias Instability (°/h, allan, typ)

≤0.05

Bias Repeatability (°/h,6per power-up)

0.5

FM Accelerometer

Range (g)

30

Full-temperature Bias (mg,3σ)

0.5

Integrated Navigation Accuracy

Self North-seeking Accuracy(°,1σ)

1secL

Pure Inertial Accuracy (1σ)

300m/300s

Combined heading accuracy (° ,1 σ, real-time)

0.5

Combined horizontal attitude (° ,1σ, real-time))

0.06

Combined horizontal position (m ,1 s)

3(single point), 0.02+1ppm (RTK)

Satellite Receiver (Built-In)

Satellite Mode

GPS:L1/L2/L5

BeiDou:B1/B2/B3

GLONASS:L1/L2

Electrical / Mechanical Interfaces

Power (V)

12~36VDC (recommended 24V)

Steady-state Power (W)

10W

Dimensions (mm×mm×mm)

65×70×63

Weight (g)

≤500

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