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{"title":"High Accuracy Ships Inertial Navigation System Widely Used Mems Inertial","imgUrl":"https:\/\/img.chinax.com\/nimg\/00\/32\/a2b4a23a38bb0f54f371accce3ef-200x200-1\/high_accuracy_ships_inertial_navigation_system_widely_used_mems_inertial_navigation_system.jpg","attrs":{"Brand Name":"Liocrebif","Model Number":"LKF-FSI301","Certification":"GJB 9001C-2017","Place of Origin":"China"}}
{"title":"High Precision Inertial Navigation Sensors MEMS Integrated Navigation System For","imgUrl":"https:\/\/img.chinax.com\/nimg\/83\/08\/fdf5d49d5e53e284d4bd7bb3436c-200x200-1\/high_precision_inertial_navigation_sensors_mems_integrated_navigation_system_for_vehicles.jpg","attrs":{"Brand Name":"Liocrebif","Model Number":"LKF-MSI300","Certification":"GJB 9001C-2017","Place of Origin":"China"}}
{"title":"Fiber Optical Inertial Guidance System 21.2*15.5*12.5cm Highly Reliable","imgUrl":"https:\/\/img.chinax.com\/nimg\/44\/d4\/8c4f0485fe3d6893b6b8c9bb918f-200x200-1\/fiber_optical_inertial_guidance_system_21_2_2a15_5_2a12_5cm_highly_reliable.jpg","attrs":{"Brand Name":"Liocrebif","Model Number":"LKF-FSI400","Certification":"GJB 9001C-2017","Place of Origin":"China"}}
{"title":"MEMS Inertial Navigation System Integrated 8.3*6.6*2.4cm For North Seeker","imgUrl":"https:\/\/img.chinax.com\/nimg\/9a\/f7\/16e12ad06b9217b7a49e8f3d8dea-200x200-1\/mems_inertial_navigation_system_integrated_8_3_2a6_6_2a2_4cm_for_north_seeker_application.jpg","attrs":{"Brand Name":"Liocrebif","Model Number":"LKF-MSI100","Certification":"GJB 9001C-2017","Place of Origin":"China"}}
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
Company Details
Bronze Gleitlager
,
Bronze Sleeve Bushings
and
Graphite Plugged Bushings
from Quality China Factory
Business Type:
Manufacturer,Exporter,Seller
Year Established:
2019
Total Annual:
6000000-7000000
Employee Number:
101~200
Ecer Certification:
Verified Supplier
COMPANY INTRODUCTION
LIOCREBIF primarily engages in the research, development, production, and distribution of various inertial navigation systems, inertial measurement units, gyroscopes, and related products, providing specialized services in the fields of inertial navigation and optoelectronic sen... COMPANY INTRODUCTION
LIOCREBIF primarily engages in the research, development, production, and distribution of various inertial navigation systems, inertial measurement units, gyroscopes, and related products, providing specialized services in the fields of inertial navigation and optoelectronic sen...