Inertial Integrated Navigation System Anti Interference | Autonomous North Seeking For Land Vehicle (RLG INS)

Product Detail

Inertial integrated navigation system anti interference | autonomous north seeking for land vehicle (RLG INS)




1. Brief introduction




The core components of LS10 Land Laser Inertial Integrated Navigation System are high precision laser gyro, quartz flexible accelerometer, accelerometer acquisition circuit, navigation computer, secondary power supply component, vibration system and so on. It can continuously and real-time provide the instant position (longitude and latitude), velocity, acceleration, heading and attitude of the vehicles, and provides detailed navigation information according to driving mission plan, can meet the requirement of most of the applications of general vehicle platforms.




2. Features




(1)Military quality


(2)Anti interference autonomous north seeking

(3)Strong ability of autonomous navigation and integrated navigation

(4)Good scalability

(5)Varied interfaces

(6)Auto Save Function




3. Performances

 

Sr. No.	Item	Grade		Remark
		A	B
system performance
1	North seeking accuracy	1mil	2mil	(1s)
2	Attitude accuracy	0.2mil	1mil	(1s)
3	North seeking time	5min	5min	(1s)
4	Course keeping/stand on accuracy	1mil/h	2mil/h
5	Pure inertial navigation accuracy	=1n mil	=1.5n mil	(1s)
6	Positioning accuracy(integrated odometer)	0.2%D	0.5%D	D means mileage (Km)
7	Horizontal positioning accuracy (Integrated GNSS)	Single point : 2m/5m(1s) DGPS:0.5m(1s) RTK:2cm+1ppm(1s)		(1s)
8	Velocity accuracy (Integrated GNSS)	0.02m/s
Core component
9	RLG bias stability	=0.01°/h	=0.02°/h	(1s)
10	RLG scale factor	2PPm	5PPm
11	Accelerometer bias stability	=0.05mg	0.1mg	(1s)

                      

4. Applications




(1). Vehicle carrier or land-based platform.

(2). Unmanned driving

(3). Mission vehicle navigation, mapping

(4). Underwater positioning navigation






5. Packages

  











E-mail: info@gyro-nav.com