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Optical Fiber Strapdown Inertial Navigation System Combined With Satellite And Laser Speed Meter

Categories Electronic Gyroscope Sensor
Brand Name: Kacise
Model Number: KsINS-120
Certification: certificate of explosion-proof, CE
Place of Origin: China (Mainland)
MOQ: 1pcs
Payment Terms: T/T, Western Union, MoneyGram
Supply Ability: 1000 Pieces per Week
Delivery Time: 5-8 working days
Packaging Details: each unit has individual box and all boxes are packed in standard packages or customers requests available
Align time: 5min
Power consumption: ≤ 20W
Operating temperature: -40℃~ +65℃
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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:

Car navigationship navigationDrone navigationShip local datum

Location (CEP)

≤ 0.1%D,

Odometer assist

≤ 0.1m,

Differential Satellite Assist

≤ 1nm/8h,

Trip meter assist

≤ 0.1m,

Differential Satellite Assist


≤ 0.8nmile/h


≤ 1m (relative)

Speed(1σ)≤ 0.2m/s≤ 0.6m/s≤ 0.8m/s≤ 0.2m/s(relative)
Heading(1σ)≤ 0.5mil≤ 0.2mil(relative)
Attitude (1σ)≤ 0.02°≤ 0.01° (relative)
Align time5min15-20min5min5min

System features:

Power consumption≤ 20W
size335mm (L) × 200mm (W) × 146mm (H)
weight12kg
Input voltage18V~32V
Operating temperature-40℃~ +65℃
Mechanical environmentimpactHalf sine wave 30g, 11ms
vibrationGJB150.16A-2009.C.3

Interface information

RS-422×2; RS-232×1;

Ethernet interface; CAN bus interface;

Odometer interface×1;Altimeter interface;Speedometer interface


Device performance :

topAccelerometer
Bias stability≤ 0.005°/h,1σOffset repeatability≤ 50μg, 1σ
Offset repeatability≤ 0.005°/h,1σBias stability≤ 100μg, 1σ
scaling factor≤ 30ppm, 1σScaling factor repeatability≤ 50ppm, 1σ
random walk≤ 0.001° / , 1σScale factor stability≤ 50ppm, 1σ

Quality Optical Fiber Strapdown Inertial Navigation System Combined With Satellite And Laser Speed Meter for sale
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