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Inertial Navigation System

High Precision Integrated Navigation System with 0.05°/h Gyro Zero-Bias Stability and 200 Hz Navigation Data Frequency

Name: High Precision Integrated Navigation System with 0.05°/h Gyro Zero-Bias Stability and 200 Hz Navigation Data Frequency
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: INS500D
Price: 5,000.00 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	INS500D
MOQ:	1
Price:	Negotiable
Payment Terms:	T/T
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

China

Certification:

Single Point Positioning Accuracy (RMS):

1.2m

RTK Positioning Accuracy (RMS):

2cm±1ppm

Loss Of Lock Positioning Accuracy (CEP):

100m/10min, 0.5nm/30min, 1.5nm/h, 2‰D

Self-navigation System:

0.05°×sec/Lati

Frequency Of Navigation Data:

200 Hz

Gyroscope Range:

400°/s

Gyro Zero-bias Stability:

0.05°/h

Packaging Details:

sponge and carton

Supply Ability:

500/month

Highlight:

200 Hz Integrated Navigation System

0.05°/h Integrated Navigation System

High Precision Integrated Navigation System

Product Description

1. Overview

The fiber-optic integrated navigation system SNC500D is based on the 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 to meet the requirements for accurate measurement of attitude, heading, position and other information in the application fields of medium and high precision mobile measurement system and large UAV.

2. Performance Index

Parameter		Technical indicators
Position accuracy	Single point (RMS)	1.2m
	RTK(RMS)	2cm+1ppm
	Lock-loss accuracy (CEP)	100m/10min 0.5nm/30min 1.5nm/h 2 ‰ D, where D is the distance travelled (optional, DVL or odometer combination)
Heading (RMS)	Self-north seeking accuracy	0.05 ° × 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	0.05°/h
	Scale factor nonlinearity	50ppm
	Angular random walk	0.02°/ √hr
Accelerometer	Range	16g
	Zero bias stability	50ug
	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

3. Overall dimensions High Precision Integrated Navigation System with 0.05°/h Gyro Zero-Bias Stability and 200 Hz Navigation Data Frequency 0

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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