High Accuracy Integrated Inertial Navigation System with Built-in MEMS Gyroscope and Accelerometer

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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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High Accuracy Integrated Inertial Navigation System with Built-in MEMS Gyroscope and Accelerometer

Brand Name	Firepower
Model Number	INS100C-C0
Certification	CE
Place of Origin	CHINA
Minimum Order Quantity	1
Price	negotiable
Payment Terms	L/C, T/T
Delivery Time	1 week for sample
Packaging Details	Sponge/Box
Gyro Range	±450°/s
Gyro Bias Stability	≤0.5°/h
Accelerometer Range	±16g
Accelerometer Bias	≤100ug
Heading Accuracy	0.1 °/L (RMS)
Attitude Accuracy	0.05°(RMS)
Horizontal Velocity Accuracy	0.05m/s
Interface	RS232/RS422
Weight	≤200g
Size	806038mm

Detailed Product Description

High Accuracy Integrated Inertial Navigation System with Built-in MEMS gyroscope and accelerometer

Product Description

INS100C-C0 integrated navigation system has built-in high performance MEMS gyroscope and accelerometer, which can receive internal 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.

Main Function

The integrated navigation system can use the satellite navigation information received internally to carry out integrated navigation, and output the information of the carrier, such as pitch, roll, heading, position, speed, time and the like; After losing the satellite signal, it outputs the position, velocity and attitude information of inertial solution, and has a certain navigation accuracy maintenance function in a short time.

Technical parameters

Project		Metrics (RMS)	Remark
Heading accuracy	Dual GNSS	0.1°	2m baseline
	Single GNSS	0.1°
	Maintain accuracy	≤0.3°	GNSS failure 0.5h
Attitude accuracy	GNSS is valid	0.05°
Attitude accuracy	Maintain accuracy	≤0.3°	GNSS failure 0.5h
Horizontal positioning accuracy	GNSS is valid	1.2m	Single point L1/L2
	GNSS is valid	2cm+1ppm	RTK
	Maintain accuracy	≤1nm	GNSS failure 10min
Horizontal velocity accuracy	GNSS is valid	0.05m/s
Gyroscope	Measuring range	±450°/s
Gyroscope	Zero bias stability	≤0.5°/h	10 s average
Accelerometer	Measuring range	±16g
Accelerometer	Zero bias stability	≤100µg	10 s average
Communication interface	RS232	Route 1	Optional CAN, odometer
Communication interface	RS422	Route 1
Electrical characteristics	Voltage	9~36VDC
	Power consumption	≤6W
	Ripple	100 mV	P-P
Structural characteristics	Size	80 mm×60mm×38mm
Structural characteristics	Weight	≤200g
Use environment	Operating temperature	-40℃~+60℃
	Storage temperature	-45℃~+70℃
	Vibration	20~2000Hz,6.06g
	Impact	30g,11ms
Reliability	MTBF	30000h
Reliability	Continuous working time	>24h

Outline Drawing

Detail Photo

Payment & Shipping

Product Tags: High Accuracy Inertial Navigation System MEMS Gyroscope Inertial Navigation System Accelerometer Inertial Navigation System

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