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Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output

Categories Inertial Navigation System
Brand Name: Firepower
Model Number: INS200A
Certification: CE
Place of Origin: CHINA
MOQ: 1
Price: negotiable
Payment Terms: L/C, T/T
Supply Ability: 500/Month
Delivery Time: 1 week for sample
Packaging Details: Sponge/Box
Gyro Range: ±500°/s
Gyro Bias Stability: ≤0.04°/h
Accelerometer Range: ±20g
Accelerometer Bias Stability: ≤50ug
Interface: CAN/RS422/Network
Power Supply: 18-36V
Weight: ≤6kg
Size: 178*178*134.5mm
Bandwidth: >300Hz
Position accuracy: ≤1.5m
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Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output

Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output

Product Description

INS200A integrated navigation system has built-in high-performance MEMS gyroscope and accelerometer, which can receive external GNSS data, realize multi-sensor fusion and integrated navigation 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 parameters


Item
Indicators


Gyro

channel
Measuring range
-500°/s ~+500°/s
Resolution
≤0.01°/h
Bias residual
-0.02°/h ~+0.02°/h
Random walk

≤0.007°/√h
Bias stability at room temperature
≤0.04°/h(1σ, 10s)
Bias stability at full
temperature
≤0.06°/h(1σ, 10s)
Normal-temperature
Bias repeatability
≤0.04°/h(1σ)
Bias repeatability at full
temperature
≤0.06°/h(1σ )
Scale factor nonlinearity
≤30ppm
Scale factor repeatability
≤30ppm(1σ)
Gyro start time
≤5s
Gyro bandwidth
>300Hz
Installation error
residual of three-axis
gyroscope

≤10"

Acceleration
channel
Measuring range
-20g ~ +20g
Bias stability at
full temperature
≤50ug(1σ)
Bias repeatability
at full temperature
≤80ug(1σ)
Add up the starting time
≤5s
Triaxial addition installation error residual
≤10"
Alignment accuracy
Alignment
accuracy
North seeking time
≤5min
Heading Angle Alignment Repeatability
≤0.08°/cosL
Pitch Alignment Repeatability
≤0.005°
Roll Angle Alignment Repeatability
≤0.005°
North-seeking mode
Optional
Integrated navigation accuracy (satellite effective)
Integrated navigation accuracy
Accuracy of course
angle measurement
≤0.06°
Accuracy of pitch
angle measurement
≤0.03°

Roll angle measurement accuracy

≤0.03°
Speed accuracy
≤0.03m/s
Position accuracy
≤1.5m
Position accuracy

≤2cm+1ppm
Inertial navigation accuracy (invalid satellite)
Integrated navigation accuracy
Accuracy of course angle maintenance
≤0.06°/h
Pitch Angle Holding Accuracy
≤0.03°/h
Accuracy of roll angle maintenance
≤0.03°/h
Pure inertial horizontal positioning accuracy
≤1.0 nautical mile H(5h)
Position positioning accuracy of odometer integrated navigation
≤0.2% (mileage greater than 3 km)

Detailed photo

Factory Photo

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