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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

Drones Inertial Navigation Systems,Fiber Optic Gyroscope Inertial Navigation Systems

Fiber Optic Gyroscope Inertial Navigation Systems

Place of Origin:

China (Mainland)

نام تجاری:

Kacise

گواهی:

certificate of explosion-proof, CE

Model Number:

KsINS-90

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جزئیات محصول
Power consumption:
≤ 20W
Operating temperature:
-40℃~ +65℃
Location (CEP):
0.1%D, Odometer assist/0.1m, Differential Satellite Assist
برجسته کردن:

Drones Inertial Navigation Systems,Fiber Optic Gyroscope Inertial Navigation Systems

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Fiber Optic Gyroscope Inertial Navigation Systems

شرایط پرداخت و حمل و نقل
Minimum Order Quantity
1pcs
Packaging Details
each unit has individual box and all boxes are packed in standard packages or customers requests available
Delivery Time
5-8 working days
Payment Terms
T/T, Western Union, MoneyGram
Supply Ability
1000 Pieces per Week
محصولات مرتبط
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86--17719566736
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توضیحات محصول

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 0

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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