Low cost MEMS Inertial Navigation System for Drone Autonomous Navigation

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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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Low cost MEMS Inertial Navigation System for Drone Autonomous Navigation

Brand Name	Firepower
Model Number	GI100C-C0
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 name	INS with MEMS
Heading accuracy	0.1deg (rms)
Attitude accuracy	0.05°deg (rms)
Accelerometer range	±16g
Accelerometer zero bias stability	≤100µg
Gyroscope range	±450°/s
Gyroscope zero bias stability	≤0.5°/h
Operating temperature	-40℃~+60℃
Voltage	9~36V
Vibration	20~2000Hz

Detailed Product Description

Low cost MEMS Inertial Navigation System for Drone Autonomous Navigation

Product Description

GI100C-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 Features

The integrated navigation system can use the satellite navigation information received internally for integrated navigation, outputting information such as pitch, roll, heading, position, speed, and time of the carrier; After losing the satellite signal, the position, velocity, and attitude information of the output inertial solution can maintain a certain degree of navigation accuracy in a short period of time.

Performance Index

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 10 min
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	Optional CAN, odometer
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

Product Structure

L80mm x W60mm x H38mm(L x W x H)

Product Tags: Low cost MEMS Inertial Navigation System MEMS Inertial Navigation System Drone Autonomous Navigation Inertial Navigation System

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