Low Cost Integrated Navigation System

Product Details
Customization: Available
Type: Integrated Navigation System
Output Signal Type: Digital Output
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Address
Floor 18th, Ruihua Builiding, No. 315, Zhongshan South Road, Qinhuai District, Nanjing, ...
International Commercial Terms(Incoterms)
FOB, EXW, CFR, CIF, CIP
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LC, T/T, Western Union, Money Gram
  • Low Cost Integrated Navigation System
  • Low Cost Integrated Navigation System
  • Low Cost Integrated Navigation System
  • Low Cost Integrated Navigation System
  • Low Cost Integrated Navigation System
  • Low Cost Integrated Navigation System
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Basic Info.

Model NO.
SK200
Measuring Shaft Quantities
10dof
Accuracy Grade
Heading 0.2°, Pitch and Roll 0.1°(1σ)
Certification
ISO
Customized
Non-Customized
Interface
Uart
Supply Voltage
SMD: 3.2 ~ 5.5 V; Evaluation Kit: 5~36V
Working Temperature
-40~85 Degrees Celsius
Weight
4 Grams
Transport Package
Carton
Specification
24*22*3.8mm
Trademark
SkyMEMS
Origin
China
HS Code
9014100000
Production Capacity
500/Month

Packaging & Delivery

Package Size
15.00cm * 15.00cm * 5.00cm
Package Gross Weight
0.400kg

Product Description

Main Features
-High Accuracy: Velocity < 0.05m/s
    Attitude (Dynamic): Heading 0.2°, Pitch and Roll 0.1°(1σ) ,Horizontal Position< 1m, Vertical Position < 1.5m (RMS)
-Bias Instability (Allan): Gyro 3°/h,Accel80ug
-Real-time Gyro and Accel Bias Tracking and Compensation
-Data Output Rate: INS 400Hz, IMU 800Hz
-Full Temperature Range Sensor Calibration
-Superior SWaPPerformance: 24×22×3.8 mm, < 4g, <445mW
-Working Temperature: -40~+85°C

High Performance GNSS -Aided Integrated Navigation System
Low Cost Integrated Navigation System
Brief Introduction
SK200 is a high-performance, surface-mount GNSS-assisted inertial navigation system (GNSS/INS) that integrates a 3-axis gyroscope, 3-axis accelerometer, 3-axis magnetometer, barometer, high-sensitivity GNSS receiver, and microprocessor. In comparison to standalone GNSS modules or Attitude and Heading Reference Systems (AHRS), SK200 employs an Extended Kalman Filter algorithm to loosely couple the position and velocity outputs from the GNSS receiver with the acceleration and angular data from MEMS inertial sensors. This fusion approach delivers precise estimates of position, velocity, and attitude, while also enhancing dynamic performance.To ensure the accurate output data, SK200 is calibrated strictly over full temperature by the factory, to reduce the effects of bias error, scale factor error, cross-axis error and temperature changes on the accuracy of MEMS inertial sensor.Additionally, SK200 integrates barometer and magnetometer outputs, providing a significant advantage in altitude and attitude measurement. Leveraging a multi-sensor data fusion algorithm and specialized processing for various scenarios, SK200 is versatile and can be applied in a wide range of applications. It is especially well-suited for unmanned aerial vehicles (UAVs), unmanned underwater vehicles (UUVs), AGV carts, robots, and more.

Technical Specifications
Parameter                      Test Conditions            Min.                 Typ                 Max.       Unit      
Attitude      
    Euler Dynamic Range     Heading and Roll                                                    ±180 °
      Pitch                                                     ±90 °
    Static Accuracy     Pitch and Roll, 1σ                              0.01 °
      Heading1, Magnetic, 1σ                                 1 °
    Dynamic Accuracy     Pitch and Roll, 1σ                               0.1 °
      Heading2, 1σ                               0.2 °
    Angular Resolution                               0.001 °
Position & Velocity                                    
    Horizontal Position Accuracy     RMS                                 1 m
    Vertical Position Accuracy     RMS                                1.5 m
    Velocity Accuracy                                 0.05 m/s
Gyroscopes      
    Range                                ±2000 °/s
    Bias Instability     Allan variance                                 3 °/h
    Noise Density                                0.003 °/s/Hz
    Cross-Axis Sensitivity                                 0.05 °
    Bandwidth                                 200 Hz
Accelerometers      
    Range                                 ±16 g
    Bias Instability     Allan variance                               0.08 mg
    Noise Density                                 0.14 mg/Hz
    Cross-Axis Sensitivity                                 ±0.05 °
    Bandwidth                                 200 Hz
Magnetometer      
    Dynamic Range                                 ±2.5 Gauss
    Noise Density                                 140 uGauss/Hz
    Cross-Axis Sensitivity                                 ±0.05 °
    Bandwidth                                 200 Hz
Barometer                        
    Pressure Range       10                                           1200 mbar
    Bandwidth                                  200 Hz
GNSS Receiver  
    Receiver Type     72 channels DMA, single band L1
    Constellations     GPS, BeiDou, Galileo, GLONASS
    Time-To-First-Fix (Cold)  
    Time-To-First-Fix (Hot)  
Interfacing  
    Output Data Rate     IMU                                               up to 800 Hz
    Output Data Rate     Position, Velocity & Attitude          up to 400 Hz
    Interface     UART
    GNSS PPS  
Electrical Features (SMD)  
    Supply Voltage     SMD: 3.2 ~ 5.5 V; evaluation kit: 5~36V
    Power Consumption     SMD: 445 mW
Environmental  
    Operating Temperature     -40°C ~ 85°C
    Storage Temperature     -40°C ~ 85°C
    Vibration Resistance     20-2000Hz, 20grms
    Shock Resistance     2000g, 0.5ms
    MTBF     > 100000 h
Physical Features (SMD)  
    Size     24 × 22 × 3.8 mm
    Weight     4 grams
Note:
    1:With proper magnetic declination, suitable magnetic environment and valid hard/soft iron calibration.
    2:With sufficient motion for dynamic alignment.
 
Typical Applications
Unmanned Aerial Vehicles
Low Cost Integrated Navigation System
 
- Unmanned Surface Vessel
Low Cost Integrated Navigation System
 
Precision Agriculture
Low Cost Integrated Navigation System
 
Industrial Robotics
Low Cost Integrated Navigation System
 
 
Product Advantages
1.High Accuracy, High Performance and Powerful Functions
Low Cost Integrated Navigation System
2.Aerospace Level Reliability, 12-step Strictest Quality Control
Low Cost Integrated Navigation System
3.Competitive Price, ODM supported
Low Cost Integrated Navigation System

4.Successful Applications in many Fields, 300+ Customers are Using
Low Cost Integrated Navigation System

5.World-class Production Line, Fast Delivery
Low Cost Integrated Navigation System

6.Service with Heart, Professional Technical Support
Low Cost Integrated Navigation System
 
 
 
 

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