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High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology

Categories Inertial Navigation System
Brand Name: Firepower
Model Number: GI100E-A0-DGI
Certification: CE ROHS
Place of Origin: CHINA
MOQ: 1
Price: negotiable
Payment Terms: T/T
Supply Ability: 500/month
Delivery Time: 10 days
Packaging Details: sponge+carton
Product name: Integrated Navigation System with Accelerometer
Heading accuracy: 0.1deg (rms)
Attitude accuracy: 0.1deg (rms)
Horizontal velocity accuracy: 0.1m/s
Gyro range: ±500°/s
Gyro zero bias stability: 4°/h
Accelerometer range: ±16g
Accelerometer zero bias stability: 0.2mg
Communication interface: RS-422/RS-232
Weight: ≤150g
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High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology

High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology


Product Description


The GI100E-A0-DGI integrated navigation system has built-in high-performance MEMS gyroscope and accelerometer, which can receive internal GNSS data, realize multi-sensor fusion and integrated navigation solution algorithm, and have short-term inertial navigation capability when GNSS is invalid.

The product has high reliability and strong environmental adaptability. By matching different software, the products can be widely used in the fields of tactical and industrial unmanned aerial vehicles, unmanned vehicles, unmanned ships, aviation guided bombs, intelligent ammunition, rockets, mobile communication, mapping, seeker and stable platform.


Technical indicators


ProjectMetrics (RMS)Remark
Heading accuracyGNSS Valid 0.1° 
Course holding0.2°/minGNSS failure
Attitude accuracyGNSS is valid0.1°Single-point L1/L2, RTK
Attitude maintenance0.2°/minGNSS failure
Positioning accuracyHorizontal, GNSS valid; RTK1.5m;1cm+1ppmSingle point L1/L2; Differential
Elevation, GNSS valid; RTK2.5m;2cm+1ppmSingle point L1/L2; Differential
Position keeping, GNSS failure20mUnlocked for 60s
Horizontal velocity accuracyGNSS is valid0.1m/sSingle-point L1/L2, RTK
GyroscopeMeasuring range±500°/s 
Zero bias stability4°/hAllan variance
AccelerometerMeasuring range±16gCustomizable 200 G
Zero bias stability0.2mgAllan variance
Satellite cardCold start< 30 secondsOpen environment
Hot start5 secondsOpen environment
Type of receiverBDS B1I/B2I/B3I 
GPS L1C/A/L2P (Y)/L2C/L5
GLONASS G1/G2
Galileo E1/E5a/E5b
QZSS L1/L2/L5
Communication interfaceRS232Route 2 
RS422Route 1 
Electrical characteristicsVoltage9~36VDC 
Power consumption≤3W 
Ripple100 mVP-P
Structural characteristicsSize80 mm×53 mm×23mm 
Weight≤150g 
Use environmentOperating temperature-40℃~+60℃ 
Storage temperature-45℃~+65℃ 
Vibration20~2000Hz,6.06g 
Impact30g,11ms 
Degree of protectionIP65 
ReliabilityMTBF30000h 
Life span> 15 years 
Continuous working time>24h 

Main Features


The integrated navigation system can carry out integrated navigation by using the satellite navigation information received internally, and output the pitch, roll, course, position, speed, time and other information of the carrier; After losing the satellite signal, it outputs the position, velocity and attitude information of inertial solution, and has a certain navigation accuracy maintenance function in a short time.


Product Dimensions



L80mm x W53mm x H23mm(L x W x H)


Quality High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology for sale
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