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MEMS Inertial Navigation System Integrated 8.3*6.6*2.4cm For North Seeker Application

Wuhan Liocrebif Technology Co., Ltd
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    Buy cheap MEMS Inertial Navigation System Integrated 8.3*6.6*2.4cm For North Seeker Application from wholesalers
     
    Buy cheap MEMS Inertial Navigation System Integrated 8.3*6.6*2.4cm For North Seeker Application from wholesalers
    • Buy cheap MEMS Inertial Navigation System Integrated 8.3*6.6*2.4cm For North Seeker Application from wholesalers
    • Buy cheap MEMS Inertial Navigation System Integrated 8.3*6.6*2.4cm For North Seeker Application from wholesalers
    • Buy cheap MEMS Inertial Navigation System Integrated 8.3*6.6*2.4cm For North Seeker Application from wholesalers

    MEMS Inertial Navigation System Integrated 8.3*6.6*2.4cm For North Seeker Application

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    Brand Name : Liocrebif
    Model Number : LKF-MSI100
    Certification : GJB 9001C-2017
    Price : 5000-25000CHY
    Payment Terms : T/T
    Supply Ability : 10000
    Delivery Time : 2-4 weeks
    • Product Details
    • Company Profile

    MEMS Inertial Navigation System Integrated 8.3*6.6*2.4cm For North Seeker Application

    Essential details
    MOQ:1
    Size:L(8.3)*W(6.6)*H(2.4) cm
    Specification Number:LKF-MSI100
    Product Introduction

    Introduction

    The MSI100 MEMS Integrated Navigation System is a highly reliable, cost-effective MEMS inertial navigation system that can be widely used in navigation, control, and measurement applications in vehicles, ships, and drones.
    The MSI100 series integrated navigation system integrates high-performance MEMS gyroscopes, MEMS accelerometers, and GNSS satellite receiver chips into its navigation calculation module. By measuring the angular velocity and acceleration of the carrier's motion, it continuously receives GNSS satellite signals via dual antennas or track angles, and calculates the current carrier's heading angle, three-dimensional velocity, position, and attitude information. The integrated navigation system has undergone full-temperature zero-point and full-temperature scale compensation for its internal IMU module, ensuring the reliability of the product.


    Technical Specification

    Liocrebif Company is a high-tech enterprise that has achieved a fully closed-loop system for fiber optic winding equipment, fiber optic winding manufacturing, IMU circuits, software, and IMU testing and calibration equipment. By comprehensively controlling upstream and downstream processes, the company can effectively improve product quality and reduce system costs. At the same time, the company implements the ISO9001 quality system and adopts strict processes to ensure the reliability and consistency of product performance.
    The products offer various configuration options to accommodate different platforms, such as airborne, vehicle-mounted, and ship-mounted applications. When vehicle-mounted, the system incorporates vehicle constraints to ensure long-term measurement accuracy of attitude.


    Table 1 Performance parameters of LKF-MSI100

    MEMS Gyroscope

    Range (°/s)

    ±500

    Full-Scale Zero Drift (°/h, 1σ)

    180(X,Y),≤30(Z)

    Zero Offset Stability (°/h, 10s Smoothing)

    10(XY),≤5(Z)

    Zero Offset Instability (°/H, Allan)

    2(XY),≤0.5(Z)

    Zero Offset Repeatability (°/h)

    10(XY),≤5(Z)

    Angular Random Walk (°/h)

    ≤0.25

    Scale Factor Nonlinearity (ppm)

    ≤100

    Cross-Coupling (Rad)

    ≤0.001

    Bandwidth (Hz)

    ≥100

    MEMS Accelerometer

    Range (G)

    ±16

    Zero Position (mg, 1σ)

    2

    Zero Offset Stability (ug, 10s Smoothing)

    ≤100

    Zero Bias Stability (ug, Allan)

    ≤50

    Zero Bias Repeatability (Ug)

    ≤100

    Velocity Random Walk (mm/s/h)

    ≤40

    Scale Factor Nonlinearity (ppm)

    ≤300

    Cross-Coupling (rad)

    0.001

    Bandwidth (Hz)

    ≥100

    Combined Navigation Accuracy

    Combined Heading (°, 1σ, Real-Time)

    0.15 (1 m baseline, dual antenna), 0.5 (single antenna, dynamic)

    Combined Horizontal Attitude (°, 1σ, Real-Time)

    0.05° (dual antenna), 0.1° (single antenna)

    Combined Horizontal Position (m, 1σ)

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

    Combined Vertical Position (m, 1σ)

    5 m (single point), 0.03+1 ppm (RTK)

    Combined Horizontal Velocity (m/S, 1σ)

    0.1

    Combined Vertical Velocity (m/S, 1σ)

    0.15

    Pure Inertial Navigation Accuracy

    Horizontal Attitude (°, 1σ, Real-Time)

    0.05° (static), 0.5° (dynamic)

    Heading (°, 1σ, Real-Time)

    5° (dynamic)

    Dead Reckoning Accuracy (cm)

    5

    Inertial/Odometer Combination Accuracy

    0.001D(60s)

    Electrical/Mechanical Interface

    Power Supply (V)

    9~36

    Steady-State Power (W)

    3

    Start-Up Time (s)

    2

    Communication Interface

    1 RS-422 channel, 1 RS-232 channel, 1 CAN channel

    1 TTL level synchronous input channel, 1 TTL level synchronous output channel

    Update Rate (Hz)

    200 (customizable)

    Dimensions (mm × mm × mm)

    83×66×24

    Weight (G)

    350

    Operating Environment

    Operating Temperature (°C)

    -40+85

    Storage Temperature (°C)

    -55+85

    Vibration (G, RMS)

    20~2000HZ,4.08

    Shock (G)

    1000g/1ms

    Reliability

    MTBF (h)

    100000


    Main Features

    Supports full GNSS frequency points, high positioning and orientation accuracy in complex environments.
    High-precision gyroscope used for heading axis, high attitude maintenance accuracy after lock loss.
    Self-correction algorithm when GNSS is unavailable, maintains horizontal attitude accuracy.
    RTK differential can be connected.
    Zero speed correction and vehicle constraint algorithm improve autonomous accuracy.
    100% domestically produced components, high performance, small size, low weight.


    Application

    UAV/Vehicle/Ship/Boat position and attitude reference
    Attitude control
    Optical/photographic platform
    Surveying and mapping
    Stabilized platform
    Underwater vehicle
    Motion communication
    Intelligent driving
    Missile control


    Fig. 1 Dimensions of the external structure

    图示, 形状, 工程绘图, 矩形 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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    MEMS Inertial Navigation System Integrated 8.3*6.6*2.4cm For North Seeker Application
    Quality MEMS Inertial Navigation System Integrated 8.3*6.6*2.4cm For North Seeker Application for sale
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