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Fiber Optic Gyroscope GNSS Integrated Inertial Navigation System for Land Vehicle

Name: Fiber Optic Gyroscope GNSS Integrated Inertial Navigation System for Land Vehicle
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: INS500D
Price: 7000 USD
Availability: InStock

Brand Name:	FIREPOWER
Model Number:	INS500D
MOQ:	1
Price:	7000$
Payment Terms:	L/C,T/T,Western Union
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

China

Heading Accuracy:

0.1°

Attitude Accuracy:

0.02° (RMS)

Horizontal Velocity Accuracy:

0.1m/s

Gyro Range:

±400°/s

Gyro Zero Bias Stability:

≤0.3°/h

Acc Range:

±16g

Acc Zero Bias Stability:

≤50ug

Power Source:

9-36V

Weight:

≤2kg

Communication Interface:

PPS, Event, RS232, RS422, CAN

Packaging Details:

sponge+box

Supply Ability:

500/month

Highlight:

Land Vehicle Inertial Navigation System

GNSS Integrated Inertial Navigation System

Fiber Optic Gyroscope Inertial Navigation System

Product Description

Product Description

The fiber-optic integrated navigation system INS500D is based on closed-loop fiber-optic gyroscope, accelerometer and high-end GNSS receiving board with high cost performance, and is realized through multi-sensor fusion and navigation calculation algorithm, which meets the requirements of accurate measurement of attitude, heading and position information in the application fields of medium and high precision mobile measurement system and large UAV.

The system has inertial/satellite integrated navigation mode and pure inertial mode.

In the inertial/satellite integrated navigation mode, the satellite positioning information received by the GNSS receiver can be used for integrated navigation, and the pitch, roll, course, position, speed, time and other information of the carrier can be output; After the signal is lost, the position, velocity and attitude calculated by inertia are output, in which the pitch and roll are required to be accurate, the course keeping function is available in a short time, and the meter-level positioning accuracy is available in a short time. In the integrated navigation mode, post-processing information can be output for post-processing software to process.

After the pure inertial mode (i.e., GPS fusion has never been performed after power-on, and if it loses lock again after fusion, it belongs to the integrated navigation mode) is started, it has accurate attitude measurement function, can output the pitch and roll heading, and the pure inertial mode can find the north statically.

Technical Parameters

Parameter		Technical indicators
Position accuracy	Single point (RMS)	1.2m
	RTK(RMS)	2cm+1ppm
	Lock-loss accuracy (CEP)	1.8nm/h 2 ‰ D, where D is the distance travelled (optional, DVL or odometer combination)
Heading (RMS)	Self-north seeking accuracy	0.1 ° × sec (Lati), 10 min alignment of stationary base; Where Lati denotes the latitude.
Heading (RMS)	Lock-loss holding accuracy	0.1°/h
Attitude (RMS)	GNSS is valid	0.02°
Attitude (RMS)	Lock-loss holding accuracy	0.05°/h
Horizontal Velocity Accuracy (RMS)	Single point L1/L2	0.1m/s
Horizontal Velocity Accuracy (RMS)	GNSS is invalid	2m/s/h
Navigation data frequency	200Hz
Gyroscope	Range	400°/s
	Zero bias stability	0.3°/h
	Scale factor nonlinearity	50ppm
	Angular random walk	0.02°/ √hr
Accelerometer	Range	16g
	Zero bias stability	50ug⑤
	Scale factor nonlinearity	100ppm
	Speed random walk	0.01m/s/ √hr
Physical dimensions and electrical characteristics	Overall dimensions	138.5 mm× 136.5 mm×102mm
	Weight	2.0 kg (without cable)
	Input voltage	12～36VDC
	Power consumption	< 24W (steady state)
	Store	16G
Environmental indicators	Operating temperature	-40℃~+60℃
	Storage temperature	-45℃~+70℃
	Random vibration	6.06g,20Hz~2000Hz
	MTBF	3000h
Interface characteristics	PPS, EVENT, RS232, RS422, CAN (optional)
	100m network port
	Antenna Connector (TNC)
	Wheel speed sensor interface

Outline Drawing

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

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Fiber Optic Gyroscope GNSS Integrated Inertial Navigation System for Land Vehicle

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