Advanced Ins Technology for Accurate Navigation

• Type: Inertial Navigation
• Output Signal Type: Digital Output
• Measuring Shaft Quantities: Three
• Accuracy Grade: 2cm
• IP Rating: IP67
• Certification: CE
• Model NO.: IMU300F
• Customized: Customized
• Positionin G Accuracy: 2cm+1ppm Gnss Valid Rtk
• Heading Accuracy: 0.1deg
• Attitude Accuracy: 0.02deg (RMS)
• Power Source: 9-36V
• Weight: <1kg
• Transport Package: Sponge and Box
• Specification: 92mm*92mm*90mm
• Trademark: AVIC
• Origin: China
• Production Capacity: 100/Month

Product Description

Advanced INS technology for accurate navigation
 

Product Description

The fiber optic integrated navigation system IMU300F-DGI is composed of three-axis closed-loop fiber optic gyroscope, accelerometer and navigation board with high cost performance, which is realized by multi-sensor fusion and navigation algorithm to meet the requirements of accurate measurement of attitude, heading, position and other information in the application fields of medium and high precision mobile measurement systems, medium and large
 

Features

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 internal 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 of the inertial solution are output, in which the pitch and roll are required to be kept accurate, with a certain course keeping function in a short time and meter-level positioning accuracy in a short time. After the pure inertial mode (that is, 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. 
 

Product Parameters

 

Project	Test conditions	Indicators
Positioning accuracy	GNSS Valid, Single Point	1.5m
	GNSS Valid, RTK	2cm+1ppm
	Pure inertial horizontal position holding	80m/5min(CEP)500m/10min(CEP)1.5nm/30min(CEP)
	Airspeed combination horizontal position hold	0.8nm/30min (CEP)
Heading accuracy	Single antenna (RMS)	0.1°
	Dual Antenna (RMS)	0.2 °/L (L = baseline length) (RMS)
	Course Keeping (RMS)	0.2°/30min(RMS),0.5°/h
	Self-north seeking accuracy (RMS)	1.0 ° SecL, 5-10 min
Attitude accuracy	GNSS is valid	0.02°(RMS)
	Attitude hold (GNSS failure)	0.2°/30min(RMS),0.5°/h(RMS)
Speed accuracy	GNSS valid, single point L1/L2	0.1m/s(RMS)
Gyroscope	Measuring range	±400°/s
	Zero bias stability	≤0.3°/h
Accelerometer	Measuring range	±20g
	Zero bias stability	≤100µg
Physical dimensions and electrical characteristics	Voltage	9-36V DC
	Power consumption	≤ 12W (steady state)
	Interface	2-channel RS232, 1-channel RS422, 1-channel PPS (LVTTL/422 level)
	Size	92.0 mm × 92.0 mm × 90.0mm (L, W, H)
	Weight	≤1.5kg
Environmental characteristics	Operating temperature	-40ºC~+60ºC
	Storage temperature	-45ºC~+70ºC
	Vibration	5 ~ 2000Hz, 6.06 G (with shock absorber)
	Impact	30g, 11 ms (with shock)
	Life span	> 15 years
	Continuous working time	>24h
Note:The alignment is valid;For airborne use, there is a turning maneuver before the airspeed combination, and the test takes the flight speed of 150km/H as an example;On-board conditions, need to be mobile;

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