Xi'an Kacise Optronics Co.,Ltd.

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

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Xi'an Kacise Optronics Co.,Ltd.
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Province/State:Shaanxi
Country/Region:china
Contact Person:MsEvelyn Wang
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Drones Inertial Navigation Systems Based On Fiber Optic Gyroscopes with power consumption ≤ 20W

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Brand Name :Kacise
Model Number :KsINS-90
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
Power consumption :≤ 20W
Operating temperature :-40℃~ +65℃
Location (CEP) :0.1%D, Odometer assist/0.1m, Differential Satellite Assist
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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.

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

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 navigation ship navigation Drone navigation Ship 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 time 5min 15-20min 5min 5min

System features:

Power consumption ≤ 20W
size 230mm (L) × 150mm (W) × 140mm (H)
weight 6kg
Input voltage 18V~32V
Operating temperature -40℃~ +65℃
Mechanical environment impact Half sine wave 30g, 11ms
vibration GJB150.16A-2009.C.3

Interface information

RS-232/RS-422×2

Built-in satellite receiver

Odometer interface; altimeter interface; speedometer interface

Device performance :

top Accelerometer
Bias stability ≤ 0.01°/h,1σ Offset repeatability ≤ 50µg, 1σ
Offset repeatability ≤ 0.01°/h,1σ Bias stability ≤ 100µg, 1σ
scaling factor ≤ 30ppm, 1σ Scaling factor repeatability ≤ 50ppm, 1σ
random walk ≤ 0.001° / , 1σ Scale factor stability ≤ 50ppm, 1σ

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