Drones Inertial Navigation Systems Based On Fiber Optic Gyroscopes with power consumption ≤ 20W

Brand Name:Kacise
Certification:certificate of explosion-proof, CE
Model Number:KsINS-90
Minimum Order Quantity:1pcs
Delivery Time:5-8 working days
Payment Terms:T/T, Western Union, MoneyGram
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Address: i City, No11, TangYan South road, Yanta District, Xi'an,Shaanxi,China.
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Product Details

KsINS-90 type optical fiber strapdown inertial navigation system


product description:


The KsINS-90 fiber optic gyroscope strapdown navigation system is based on a universal fiber optic inertial navigation platform. The platform adopts a universal design concept and is easy to make adaptive changes according to user needs. It has the advantages of short development cycle, high maturity, and good reliability. ; Its supporting gyroscopes, accelerometers, circuits and other components are all made from our existing shelf products, which are mature and reliable.

Features:


● Using domestic fiber optic gyroscope and quartz flexible accelerometer

● The bias stability of type 90 fiber optic gyroscope is better than 0.01°/h (1σ)

● Accelerometer bias stability is better than 50µg (1σ)

● Compatible with static and dynamic base alignment methods, self-alignment and transfer alignment can be selected according to user needs

● Can integrate navigation with external information such as satellite navigation instrument, speedometer, odometer, altimeter, etc., with 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/5h,

Trip meter assist

≤ 0.1m,

Differential Satellite Assist


≤ 1nmile/h


≤ 1m (relative)

Speed(1σ)≤ 0.3m/s≤ 1.0m/s≤ 1.0m/s≤ 0.2m/s(relative)
Heading(1σ)≤ 1.0mil≤ 0.5mil(relative)
Attitude (1σ)≤ 0.02°≤ 0.01° (relative)
Align time5min15-20min5min5min

System features:


Power consumption≤ 20W
size230mm (L) × 150mm (W) × 140mm (H)
weight6kg
Input voltage18V~32V
Operating temperature-40℃~ +65℃
Mechanical environmentimpactHalf sine wave 30g, 11ms
vibrationGJB150.16A-2009.C.3

Interface information

RS-232/RS-422×2

Built-in satellite receiver

Odometer interface; altimeter interface; speedometer interface

Device performance :


topAccelerometer
Bias stability≤ 0.01°/h,1σOffset repeatability≤ 50µg, 1σ
Offset repeatability≤ 0.01°/h,1σBias stability≤ 100µg, 1σ
scaling factor≤ 30ppm, 1σScaling factor repeatability≤ 50ppm, 1σ
random walk≤ 0.001° / , 1σScale factor stability≤ 50ppm, 1σ

China Drones Inertial Navigation Systems Based On Fiber Optic Gyroscopes with power consumption ≤ 20W supplier

Drones Inertial Navigation Systems Based On Fiber Optic Gyroscopes with power consumption ≤ 20W

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