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

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

Brand Name Kacise
Model Number KsINS-90
Certification certificate of explosion-proof, CE
Place of Origin China (Mainland)
Minimum Order Quantity 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
Power consumption ≤ 20W
Operating temperature -40℃~ +65℃
Location (CEP) 0.1%D, Odometer assist/0.1m, Differential Satellite Assist
Detailed Product Description

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
 

 

Product Tags: Drones Inertial Navigation Systems   Fiber Optic Gyroscope Inertial Navigation Systems  
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