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Low Cost Inertial Heading 9 Axis Navigation Sensor Navigational Guided System

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Low Cost Inertial Heading 9 Axis Navigation Sensor Navigational Guided System
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Features
Specifications
Product: FOG INS
Gyro Range: 300°/s
Gyro Resolution: ≤0.5°/h
Gyro Bias: ±1.0°/h
Gyro Bias Stability: ≤0.3°/h(1σ)
Accelerometer Range: ±50g
Scale Factor: ≤300ppm
Random Walk: ≤0.02m/s/h1/2
High Light:

9 Axis Navigation Sensor

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Inertial Heading Navigation Sensor

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ROHS Inertial Navigation System

Basic Infomation
Place of Origin: CHINA
Brand Name: avic
Certification: CE ROHS
Model Number: INS100
Payment & Shipping Terms
Packaging Details: sponge+carton
Delivery Time: 10 days
Payment Terms: T/T
Supply Ability: 500/month
Product Description

Navigational Guided System Low Cost Inertial Heading System 9 Axis Navigational Sensor

 

 

Gyro specs

Project Indicators Remark

 

 

 

Gyro channel

Measuring range -300°/s ~+300°/s  
Resolution ≤0.5°/h  
Zero-bias residual -1.0°/h ~+1.0°/h  
Random walk 0.05 o / h  
Zero bias stability at room temperature ≤0.3°/h(1σ) 10 seconds smoothing, 1H test result
Zero bias stability at full temperature ≤0.5°/h(1σ) 10 seconds smoothing, 1H test result
Normal-temperature zero-bias repeatability ≤0.3°/h(1σ) Statistics of 6 test data
Zero-bias repeatability at full temperature ≤0.5°/h(1σ)

Take 2 zero-bias data at full temperature,

high temperature, low temperature and

normal temperature respectively

Scale factor nonlinearity ≤300ppm Full temperature and constant temperature
Scale factor repeatability ≤300ppm(1σ) Full temperature and constant temperature
  Gyro start time ≤5s  
  Gyro bandwidth 300Hz Design assurance, batch testing
  Installation error residual of three-axis gyroscope ≤30"  
 

acc specs

Project Indicators Remark

 

 

Acceleration channel

Measuring range -50g ~ +50g Design and selection guarantee
Scale factor nonlinearity ≤300ppm Design and selection guarantee
Zero bias stability at full temperature ≤100ug(1σ) 10 seconds smoothing, 1H test result
Zero-bias repeatability at full temperature ≤100ug(1σ)

Take 2 zero-bias data at full temperature, high temperature,

low temperature and normal temperature respectively

Scale factor repeatability ≤100ppm(1σ) Design and selection guarantee
Random walk ≤0.02m/s/h1/2  
  Add up the starting time ≤5s  
  Triaxial addition installation error residual ≤30"  
 

INS-100 is a high-precision integrated navigation system independently developed by AVIC group. It is equipped with

three self-developed 40 fiber optic gyroscopes, three-self MEMS accelerometers and GNSS modules, and realizes

high-precision positioning and navigation in complex environments through multi-sensor fusion and integrated

navigation algorithm. The product has high reliability and strong environmental adaptability. The products can be

widely used in intelligent driving, UAV, surveying and mapping, marine compass, stable platform, photoelectric pod,

underwater vehicle and other fields.

 

Low Cost Inertial Heading 9 Axis Navigation Sensor Navigational Guided System 0

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