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Fiber Optic Gyroscope Inertial Navigation System with ≤ 20W Power Consumption, 0.01°/h Bias Stability, and -40℃ to +65℃ Operating Temperature

Fiber Optic Gyroscope Inertial Navigation System with ≤ 20W Power Consumption, 0.01°/h Bias Stability, and -40℃ to +65℃ Operating Temperature

Drones Inertial Navigation Systems

Fiber Optic Gyroscope Inertial Navigation Systems

Place of Origin:

China (Mainland)

Brand Name:

Kacise

Certification:

certificate of explosion-proof, CE

Model Number:

KsINS-90

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Product Details
Power Consumption:
≤ 20W
Operating Temperature:
-40℃~ +65℃
Operating Temperature:
-40℃~ +65℃
Location (CEP):
0.1%D, Odometer Assist/0.1m, Differential Satellite Assist
Highlight:

Drones Inertial Navigation Systems

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Fiber Optic Gyroscope Inertial Navigation Systems

Payment & Shipping Terms
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
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.

Fiber Optic Gyroscope Inertial Navigation System with ≤ 20W Power Consumption, 0.01°/h Bias Stability, and -40℃ to +65℃ Operating Temperature 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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