Optical Fiber Strapdown Inertial Navigation System Combined With Satellite And Laser Speed Meter
|
KsINS-120 fiber optic strapdown inertial navigation system product description: The KsINS-120 fiber optic gyro strapdown navigation system is based on our institute's fiber optic inertial navigation universal platform. This platform adopts a universal design concept and is easy to make adaptive changes according to user needs. It has a short development cycle, high maturity and good reliability. and other advantages; its supporting gyroscopes, accelerometers, analog-to-digital conversion circuits, navigation computers and other components are all products on our shelves, which are mature and reliable. Features: ● Using domestic 120 type fiber optic gyroscope and quartz flexible accelerometer ● The bias stability of the 120 type fiber optic gyroscope is better than 0.005°/h (1σ) ● Accelerometer bias stability is better than 50μg (1σ) ● Achieve static and dynamic base alignment, and can choose self-alignment or on-the-fly alignment according to user needs ● It can be integrated with various information such as satellites, laser speedometers, odometers, altimeters, etc. for combined navigation, and the interface has strong scalability
Application fields and application modes: Land use, navigation, drones, and can also be extended to other applications.
System performance:
System features:
Device performance :
|
|||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
Product Tags: Satellite Inertial Navigation System Laser Speed Meter Inertial Navigation System |
![]() |
Dynamically Tuned Gyroscope For Well Logging for Temperature Sensor |
![]() |
Well Logging Dynamically Tuned Gyroscope For High Temperature Environment |
![]() |
Single Axis Fiber Optic Electronic Gyroscope Sensor Shocking Resistance |
![]() |
Gyroscope/Angular velocity sensor/Used to measure the angular velocity in the direction of the sensitive axis |
![]() |
AI vision inertial navigation system for aircraft lifting assistance with weight ≤2.0kg |
![]() |
State-of-the-Art Inertial Navigation System Aviation for Aviation Applications with Navigation accuracy (takeoff) 1.0m |