Closed Loop Optical Fiber Integrated Inertial Navigation System Mobile Measurement

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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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Closed Loop Optical Fiber Integrated Inertial Navigation System Mobile Measurement

Brand Name	Firepower
Model Number	GI300F
Certification	CE ROHS
Place of Origin	CHINA
Minimum Order Quantity	1
Price	negotiable
Payment Terms	T/T
Supply Ability	500/month
Delivery Time	10 days
Packaging Details	sponge+carton
Product	FOG INS
Heading accuracy	0.1°
Attitude accuracy	0.02°（RMS）
Gyroscope range	±400°/s
Zero bias stability	≤100µg
Accelerometer range	±20g

Detailed Product Description

Closed-Loop Optical Fiber Integrated Navigation System High Precision Mobile Measurement Systems

The fiber-optic integrated navigation system GI300F-INS is based on closed-loop fiber-optic gyroscope and accelerometer with high cost performance, and is realized through multi-sensor fusion and navigation calculation algorithm, which meets the requirements of precise measurement of attitude, heading and position information in the application fields of medium and high precision mobile measurement systems, medium and large UAVs, etc.

Project	Test conditions	Indicators
Positioning accuracy	External GNSS Valid, Single Point	Better than external satellite positioning accuracy
	External GNSS Valid, RTK	Better than external satellite positioning accuracy
	Pure inertial horizontal position holding①	80m/5min(CEP) 500m/10min(CEP) 1.5nm/30min(CEP)
	Airspeed combination horizontal position hold②	0.8nm/30min (CEP)
Heading accuracy	Single antenna (RMS)	0.1°③
	Dual Antenna (RMS)	0.2 °/L (L = baseline length) (RMS)
	Course Keeping (RMS)	0.2°/30min(RMS),0.5°/h
	Self-north seeking accuracy (RMS)	0.2 ° SecL, dual position alignment for 15 min 1.0 ° SecL, single position alignment 5-10 min
Attitude accuracy	GNSS is valid	0.02°(RMS)
Attitude accuracy	Attitude hold (GNSS failure)	0.2°/30min(RMS),0.5°/h(RMS)
Speed accuracy	GNSS valid, single point L1/L2	0.1m/s(RMS)
Gyroscope	Measuring range	±400°/s
Gyroscope	Zero bias stability	≤0.3°/h
Accelerometer	Measuring range	±20g
Accelerometer	Zero bias stability	≤100µg
Physical dimensions and electrical characteristics	Voltage	9-36V DC
	Power consumption	≤ 12W (steady state)
	Interface	2-channel RS232, 1-channel RS422, 1-channel PPS (LVTTL/422 level)
	Size	92.0 mm × 92.0 mm × 81.0mm (L, W, H)
	Weight	≤1.2kg
Environmental characteristics	Operating temperature	-40℃~+60℃
	Storage temperature	-45℃~+70℃
	Vibration	5 ~ 2000Hz, 6.06 G (with shock absorber)
	Impact	30g, 11 ms (with shock)
	Life span	> 15 years
	Continuous working time	>24h
Height limit ≤5000m
speed limit ≤500m/s
Note: The alignment is valid; For airborne use, there is a turning maneuver before the airspeed combination, and the test takes the flight speed of 150km/H as an example; On-board conditions, need to be mobile;

Size:

Product Tags: Closed Loop Inertial Navigation System FOG INS Inertial Navigation System High Precision Inertial Navigation System

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