Unmanned Vehicles and Ships Integrated Navigation System Gyro with High Heading Accuracy

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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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Unmanned Vehicles and Ships Integrated Navigation System Gyro with High Heading Accuracy

Brand Name	Firepower
Model Number	INS200A
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	Sponge/Box
Gyro Range	±500°/s
Gyro Bias Stability	≤0.04°/h
Accelerometer Range	±20g
Accelerometer Bias Stability	≤50ug
Weight	≤6kg
Size	178178134.5mm
Interface	CAN/RS422/Network
Power Supply	18-36V
Bandwidth	>300Hz
Position accuracy	≤1.5m

Detailed Product Description

Unmanned Vehicles and Ships Integrated Navigation System Gyro with High Heading Accuracy

Product Description

INS200A integrated navigation system has built-in high-performance MEMS gyroscope and accelerometer, which can receive external GNSS data, realize multi-sensor fusion and integrated navigation algorithm, and have short-term inertial navigation capability when GNSS is invalid.

The product has high reliability and strong environmental adaptability. By matching different
software, the products can be widely used in the fields of tactical and industrial unmanned aerial vehicles, unmanned vehicles, unmanned ships, aviation guided bombs, intelligent ammunition, rockets, mobile communication, mapping, seeker and stable platform.

Technical parameters

Item		Indicators
Gyro channel	Measuring range	-500°/s ～+500°/s
	Resolution	≤0.01°/h
	Bias residual	-0.02°/h ～+0.02°/h
	Random walk	≤0.007°/√h
	Bias stability at room temperature	≤0.04°/h(1σ, 10s)
	Bias stability at full temperature	≤0.06°/h(1σ, 10s)
	Normal-temperature Bias repeatability	≤0.04°/h(1σ)
	Bias repeatability at full temperature	≤0.06°/h(1σ )
	Scale factor nonlinearity	≤30ppm
	Scale factor repeatability	≤30ppm(1σ)
	Gyro start time	≤5s
	Gyro bandwidth	>300Hz
	Installation error residual of three-axis gyroscope	≤10"
Acceleration channel	Measuring range	-20g ～ +20g
	Bias stability at full temperature	≤50ug(1σ)
	Bias repeatability at full temperature	≤80ug(1σ)
	Add up the starting time	≤5s
	Triaxial addition installation error residual	≤10"

Alignment accuracy
Alignment accuracy	North seeking time	≤5min
	Heading Angle Alignment Repeatability	≤0.08°/cosL
	Pitch Alignment Repeatability	≤0.005°
	Roll Angle Alignment Repeatability	≤0.005°
	North-seeking mode	Optional

Integrated navigation accuracy (satellite effective)
Integrated navigation accuracy	Accuracy of course angle measurement	≤0.06°
	Accuracy of pitch angle measurement	≤0.03°

	Roll angle measurement accuracy	≤0.03°


	Speed accuracy	≤0.03m/s
	Position accuracy	≤1.5m
	Position accuracy	≤2cm+1ppm

Inertial navigation accuracy (invalid satellite)
Integrated navigation accuracy	Accuracy of course angle maintenance	≤0.06°/h
	Pitch Angle Holding Accuracy	≤0.03°/h
	Accuracy of roll angle maintenance	≤0.03°/h
	Pure inertial horizontal positioning accuracy	≤1.0 nautical mile H(5h)
	Position positioning accuracy of odometer integrated navigation	≤0.2% (mileage greater than 3 km)

Detailed photo

Factory Photo

Payment & Shipping

Product Tags: Ships Integrated Navigation System Gyro High Heading Accuracy Gyro Vehicles Integrated Navigation System Gyro

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