Name: Precise Navigation Sensor Integrated Navigation System with GPS Accurate Attitude Angle Sensor
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: INS100C-C0
Price: Negotiable USD
Availability: InStock

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Features

Specifications

Heading Accuracy: 0.1 °/L (RMS)

Attitude Accuracy: 0.05°(RMS)

Horizontal Velocity Accuracy: 0.05m/s

Gyro Range: ±450°/s

Gyro Bias Stability: ≤0.5°/h

Accelerometer Range: ±16g

Accelerometer Bias Stability: ≤100ug

Interface: RS232/RS422

Weight: ≤200g

Size: 80*60*38mm

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Precise Navigation Sensor Integrated Navigation System

Integrated Navigation System with GPS

Basic Infomation

Place of Origin: CHINA

Brand Name: Firepower

Certification: CE

Model Number: INS100C-C0

Payment & Shipping Terms

Packaging Details: Sponge/Box

Delivery Time: 1 week for sample

Payment Terms: L/C, T/T

Supply Ability: 500/Month

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Precise Navigation Sensor Integrated Navigation System with GPS Accurate Attitude Angle Sensor

Product Description

Precise Navigation Sensor Integrated Navigation System with GPS Accurate Attitude Angle Sensor

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

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Contact Person :	Caine
Tel :	008616675562497

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