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Fiber Optical Inertial Guidance System 21.2*15.5*12.5cm Highly Reliable

    Buy cheap Fiber Optical Inertial Guidance System 21.2*15.5*12.5cm Highly Reliable from wholesalers
     
    Buy cheap Fiber Optical Inertial Guidance System 21.2*15.5*12.5cm Highly Reliable from wholesalers
    • Buy cheap Fiber Optical Inertial Guidance System 21.2*15.5*12.5cm Highly Reliable from wholesalers
    • Buy cheap Fiber Optical Inertial Guidance System 21.2*15.5*12.5cm Highly Reliable from wholesalers

    Fiber Optical Inertial Guidance System 21.2*15.5*12.5cm Highly Reliable

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    Brand Name : Liocrebif
    Model Number : LKF-FSI400
    Certification : GJB 9001C-2017
    Price : 5000-25000CHY
    Payment Terms : T/T
    Supply Ability : 10000
    Delivery Time : 2-4 weeks
    • Product Details
    • Company Profile

    Fiber Optical Inertial Guidance System 21.2*15.5*12.5cm Highly Reliable

    Essential details
    MOQ:1
    Size:L(21.2)*W(15.5)*H(12.5) cm
    Specification Number:LKF-FSI400
    Product Introduction

    Introduction

    The FSI400 Fiber-Optic Gyro-Inertial/Satellite Integrated Navigation System is a highly reliable and cost-effective navigation system suitable for a wide range of applications, including navigation, control, and measurement in fields such as aircraft, unmanned vehicles, unmanned boats, and drones.
    The integrated navigation system adopts the modular design philosophy of similar products, incorporating high-precision closed-loop fiber optic gyroscopes (FOG) and high-precision accelerometers, combined with high-performance GNSS boards. The hardware circuitry is designed using an FPGA+DSP architecture. Through multi-sensor fusion algorithms, GPS position and velocity data are input into the filter, while INS position, velocity, and attitude data are also used as filter inputs. The filter compares the differences between the two sets of data to establish an error model for estimating INS errors, and uses these errors to correct the inertial navigation results, thereby obtaining the combined navigation results for velocity, position, and attitude. The inertial navigation system offers different configuration modes to suit various platforms, such as airborne, vehicle-mounted, and ship-mounted applications. When vehicle-mounted, vehicle constraints are incorporated. Through error estimation and correction, the system achieves long-term high-precision navigation and positioning functionality for the platform.


    Technical Specification

    The integrated navigation system integrates high-precision fiber optic gyroscopes and accelerometers within an independent structure. The gyroscopes and accelerometers selected for the system represent the leading level of process inertial components in the industry. The system has undergone full temperature parameter compensation for zero position, scale factor, non-orthogonal error, and acceleration-related items, enabling it to maintain high measurement accuracy over extended periods.
    The series of integrated navigation systems can be customized with different hardware and software configurations to meet user requirements. For specific navigation applications, the gyroscope can be replaced with a high-precision gyroscope to maximize flexibility and meet the diverse needs of different users.


    Table 1 Performance parameters of LKF-FSI400

    Fiber Optical Gyroscope

    Range (°/s)

    ±300

    Zero offset (°/h)

    0.01

    Zero offset stability (°/h, 10s)

    0.01

    Zero offset instability (°/h, Allan)

    0.001

    Zero offset repeatability (°/h, 6 power-ups)

    0.01

    Angular random walk (°/√h)

    0.0005

    Scale nonlinearity (ppm)

    10

    Scale asymmetry (ppm)

    10

    Scale repeatability (ppm)

    10

    Cross-coupling (rad)

    ≤0.001

    Bandwidth (Hz)

    ≥200

    Quartz accelerometer

    Range (g)

    ±20

    Zero position (mg, 1σ)

    ≤ 0.1

    Zero offset stability (ug, 10s smoothing)

    10

    Zero bias stability (ug, Allan)

    5

    Zero bias repeatability (ug)

    10

    Velocity random walk (mm/s/√h)

    5

    Scale factor nonlinearity (mg, ppm)

    5

    Cross-coupling (rad)

    10

    Bandwidth (Hz)

    ≥200

    Pure inertial navigation accuracy

    Self-alignment accuracy (°, 1σ)

    0.06

    Attitude alignment accuracy (°, 1σ)

    0.005

    Heading hold (°, 1σ)

    0.06

    Attitude hold (°/h, 1σ)

    0.03

    Horizontal velocity (m/s, 1σ)

    0.3

    Pure inertial navigation accuracy (1σ)

    1n mile/h

    Depth measurement accuracy (cm)

    5

    Inertial/odometer combination accuracy

    ≤0.002D

    Combined navigation accuracy

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

    0.03

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

    0.01

    Combined heading accuracy (°, post-processing)

    0.003

    Combined horizontal attitude (°, post-processing)

    0.001

    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

    Timing accuracy

    20ns

    Positioning time

    ≤40s

    Start-up time

    ≤2s

    Positioning data update rate

    10Hz

    Operating altitude

    10000m

    Satellite mode

    GPS:L1/L2/L5

    BeiDou:B1/B2/B3

    GLONASS:L1/L2.

    Electrical/mechanical interface

    Input voltage

    1236VDC(Suggest 24V)

    Power consumption

    ≤18W

    Dimensions

    212 × 155 × 125 mm

    Weight

    ≤5kg

    Operating environment

    Operating temperature

    -40°C ~ +70°C

    Storage temperature

    -55°C ~ +85°C

    Vibration

    6 g @ 20~2000 Hz

    Shock

    100 g, 11 ms

    Reliability/suitability

    MTBF/MTTR

    10000 h / 0.5 h

    Maintenance

    BIT 95%



    Main Features

    Domestic core components, high performance, modular, low weight
    Supports full GNSS frequency points, high positioning and orientation accuracy in complex environments
    Rich interfaces and isolation measures
    Steady-state power consumption of 18W
    Full temperature calibration compensation from -45°C to +65°C
    Combined navigation products support automatic north seeking, with accuracy better than 1 mil°
    Built-in adaptive navigation algorithm


    Application

    Mobile measurement of position and attitude reference
    Unmanned vehicles, unmanned ships/boats
    Surveying and mapping
    Stable platforms
    Underwater vehicles
    Motion communication
    Intelligent driving
    Airborne control
    Intelligent mining North seeking


    Fig. 1 Dimensions of the external structure

    图示 AI 生成的内容可能不正确.图示 AI 生成的内容可能不正确.


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    Quality Fiber Optical Inertial Guidance System 21.2*15.5*12.5cm Highly Reliable for sale
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