Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation

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Shenzhen Fire Power Control Technology Co., LTD

City: shenzhen

Province/State:guangdong

Country/Region:china

Tel:86-755-23097872

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Fiber Optic Integrated Inertial Navigation System For Unmanned Ship Navigation

Brand Name	Firepower
Model Number	INS300
Certification	CE
Place of Origin	CHINA
Minimum Order Quantity	1
Price	negotiable
Payment Terms	L/C, T/T
Supply Ability	500/Month
Delivery Time	1 week for sample
Packaging Details	Wooden Box
Product Name	Fiber optic inertial navigation system
Gyro Range	±500°/s
Gyro Zero Bias Stability	±0.02°/h
Random Walk	≤0.0015°/√h
Gyro Bandwidth	>300Hz
Acc Range	±20g
Acc Zero Bias Stability	≤50ug
Scale factor nonlinearity	≤5ppm

Detailed Product Description

Fiber Optic Integrated Inertial Navigation System for Unmanned Ship Navigation

Product Description

INS300 is a high-precision integrated navigation system independently developed by AVIC. It contains three self-developed 98 fiber optic gyroscopes, three quartz accelerometers, high-precision sampling circuit, navigation computer circuit, GNSS module and power circuit. And high-precision position and navigation in a complex environment are realized through multi-sensor fusion and an integrated navigation algorithm. The product has high reliability and strong environmental adaptability. The products can be widely used in intelligent driving, unmanned aerial vehicle, surveying and mapping, marine compass, stable platform, underwater vehicle, roadheader, mining machinery and other fields.

Main Parameters

Project		Indicators	Remark
Gyro channel	Measuring range	-500°/s ~+500°/s
	Resolution	≤0.01°/h
	Zero-bias residual	-0.02°/h ~+0.02°/h
	Random walk	≤0.0015°/√h
	Zero bias stability at room temperature	≤0.01°/h(1σ,10s)	10 seconds smoothing, 1H test result
	Zero bias stability at full temperature	≤0.015°/h(1σ,10s)	10 seconds smoothing, 1H test result
	Normal-temperature zero-bias repeatability	≤0.01°/h(1σ)	Statistics of 6 test data
	Zero-bias repeatability at full temperature	≤0.015°/h(1σ)	Take 2 zero-bias data at full temperature, high temperature, low temperature and normal temperature respectively
	Scale factor nonlinearity	≤5ppm	Full temperature and constant temperature
	Scale factor repeatability	≤5ppm(1σ)	Full temperature and constant temperature
	Gyro start time	≤5s
	Gyro bandwidth	>300Hz	Design assurance, batch testing
	Installation error residual of three-axis gyroscope	≤10"


Acceleration channel	Measuring range	-20g ~ +20g	Design and selection guarantee
	Zero bias stability at full temperature	≤50ug(1σ)	10 seconds smoothing, 1H test result
	Zero-bias repeatability at full temperature	≤80ug(1σ)	Take 2 zero-bias data at full temperature, high temperature, low temperature and normal temperature respectively
	Add up the starting time	≤5s
	Triaxial addition installation error residual	≤10"

Product Tags: Unmanned Ship Inertial Navigation System Fiber Optic Inertial Navigation System Integrated Inertial Navigation System

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