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Home Products

Inertial Navigation System

Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance

Name: Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: INS300
Price: 5,000.00 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	INS300
MOQ:	1
Price:	negotiable
Payment Terms:	T/T
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Certification:

CE ROHS

Product:

FOG INS

Gyro Range:

500°/s

Gyro Resolution:

≤0.01°/h

Gyro Bias:

±0.02°/h

Gyro Bias Stability:

≤0.01°/h（1σ）

Accelerometer Range:

±20g

Zero Bias Stability:

≤80ug（1σ）

Zero-bias Repeatability:

≤80ug（1σ）

Packaging Details:

sponge+carton

Supply Ability:

500/month

Highlight:

FOG INS Navigation System

Nine Axis Output Navigation System

Airplane Inertial Navigation System

Product Description

Combined Navigation System Nine Axis Output For Airplan Ship Vehicle Navigation Guidance

Gyro specs

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"

acc specs

Project		Indicators	Remark
Acceleration channel	Measuring range	-20g ～ +20g	Design and selection guarantee
	Zero bias stability at full temperature	≤80ug(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"

Introduction

INS-300 is a high-precision integrated navigation system independently developed by Avic group.

It contains three self-developed 98 fiber optic gyroscopes, three quartz accelerometers, high-precision

sampling circuit, navigation computer circuit, GNSS module and power supply 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.

Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance 0

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

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Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance

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