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High Heading Accuracy 0.1° GNSS Integrated lnertial Navigation System for Marine Navigation

Name: High Heading Accuracy 0.1° GNSS Integrated lnertial Navigation System for Marine Navigation
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:

0.1° GNSS Integrated lnertial Navigation System

lnertial Navigation System for Marine Navigation

Product Description

Product Description

The INS500D fiber - optic integrated navigation system is a cost - effective solution. It is built upon a closed - loop fiber - optic gyroscope, an accelerometer, and a high - end GNSS receiving board. Through multi - sensor fusion and advanced navigation calculation algorithms, it meets the demands for precise measurement of attitude, heading, and position information in medium - to - high - precision mobile measurement systems and large - scale UAV applications.

This system supports two operation modes: inertial/satellite integrated navigation mode and pure inertial mode.

Inertial/Satellite Integrated Navigation Mode:
In this mode, the GNSS receiver utilizes the received satellite positioning information for integrated navigation. It can output information such as the carrier's pitch, roll, course, position, speed, and time. In case of signal loss, it switches to outputting position, velocity, and attitude data calculated through inertial means. The pitch and roll measurements remain accurate. There is also a short - term course - keeping function, along with short - term meter - level positioning accuracy. Additionally, in the integrated navigation mode, post - processing information can be provided for use by post - processing software.

Pure Inertial Mode:
Once the pure inertial mode is initiated (meaning that GPS fusion has not occurred since power - on; if it loses lock after prior fusion, it reverts to the integrated navigation mode), the system offers an accurate attitude measurement function. It can output pitch, roll, and heading data. Moreover, in the pure inertial mode, the system is capable of static north - finding.

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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