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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

Brand Name : Firepower

Model Number : INS100

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 : 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

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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


Product Tags:

9 Axis Navigation Sensor

      

Inertial Heading Navigation Sensor

      

ROHS Inertial Navigation System

      
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