Name: Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: INS200A
Price: Negotiable USD
Availability: InStock

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Features

Specifications

Gyro Range: ±500°/s

Gyro Bias Stability: ≤0.04°/h

Accelerometer Range: ±20g

Accelerometer Bias Stability: ≤50ug

Interface: CAN/RS422/Network

Power Supply: 18-36V

Weight: ≤6kg

Size: 178*178*134.5mm

Bandwidth: >300Hz

Position Accuracy: ≤1.5m

Highlight:

RS422 Inertial Navigation System

Precision Inertial Navigation System

Fiber Optic Gyroscope Inertial Navigation System

Basic Infomation

Place of Origin: CHINA

Brand Name: Firepower

Certification: CE

Model Number: INS200A

Payment & Shipping Terms

Packaging Details: Sponge/Box

Delivery Time: 1 week for sample

Payment Terms: L/C, T/T

Supply Ability: 500/Month

Gallery

Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output

Product Description

Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output

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

Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output 0

Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output 1

Factory Photo

Payment & Shipping

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Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output 4

Precision Inertial Navigation System ±500°/s Range with Fiber Optic Gyroscope Sensors RS422 Output 5

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Contact Person :	Caine
Tel :	008616675562497

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