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  • NTFOG150A Single-Axis Fiber Optic Gyroscope
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  • NTFOG150A Single-Axis Fiber Optic Gyroscope

    Product Model: NTFOG150A

     

    Product Overview:

     

    NTFOG150A single-axis fiber optic gyroscope (FOG) is a standardized low-precision closed-loop FOG, primarily engineered for electro-optical (EO/IR) gimbals, strapdown inertial navigation systems (SINS), inertial measurement units, optical stabilization platforms, and surveying instruments to measure angular velocity along its sensitive axis. This device delivers compact packaging, lightweight construction, wide dynamic range, and high-speed data updating capabilities.

     

    CLASSIFICATION SINGLE-AXIS FIBER OPTIC GYROSCOPE (FOG)

     

    TABSINGLE-AXIS FIBER OPTIC GYROSCOPE (FOG), Zero-bias stability≤0.2°/h(with 10-second averaging),

     

    WhatsApp: +43 67844091116

    Tel: +86 18608017948(WeChat)

    E-mail: marketing@newtron-tech.com

     



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Description

Product Model: NTFOG150A

 

Product Overview:

 

NTFOG150A single-axis fiber optic gyroscope (FOG) is a standardized low-precision closed-loop FOG, primarily engineered for electro-optical (EO/IR) gimbals, strapdown inertial navigation systems (SINS), inertial measurement units, optical stabilization platforms, and surveying instruments to measure angular velocity along its sensitive axis. This device delivers compact packaging, lightweight construction, wide dynamic range, and high-speed data updating capabilities.

 

CLASSIFICATION SINGLE-AXIS FIBER OPTIC GYROSCOPE (FOG)

 

TABSINGLE-AXIS FIBER OPTIC GYROSCOPE (FOG), Zero-bias stability≤0.2°/h(with 10-second averaging),

 

WhatsApp: +43 67844091116

Tel: +86 18608017948(WeChat)

E-mail: marketing@newtron-tech.com

 




KEY  FEATURE

 

- Bias Stability ≤0.1°/h:Enables ICBM guidance (cumulative error <100m/10,000km)

- Nonlinearity ≤50 ppm:Critical for satellite optical payload stabilization

- -45°C~+65°C Operation:Certified for Arctic warfare systems (e.g., Svalbard deployments)

- 160g Weight:Reduces UAV payload by 40% vs. legacy FOGs

- Military-Grade Ruggedness

 

APPLICATION  SCENARIOS

 

- Electro-Optical Gimbals

- Strapdown Inertial Navigation Systems (Sins)

- Inertial Measurement Units (Imus)

- Optical Platform Stabilization Devices

- Inertial Surveying Instruments To Measure Angular Velocity Along The Product's Sensitive Axis

 

PRIMARY  FUNCTIONS

 

- Angular velocity measurement

- Attitude stabilization

- Navigation reference

- Harsh environments


SPECIFICATIONS

 

Table1: Basic Parameters

Performance Parameters

NTFOG150A

Zero-Bias Stability

≤0.2°/h(with 10-second averaging)

Zero Bias Repeatability

≤0.2°/h

Random Walk Coefficient

<0.01°/√h

Scale Factor Nonlinearity

≤50ppm

Scale Factor Repeatability

≤50ppm

Operating Temperature

-45°C ~ +65°C

Dynamicrange

≥±800°/s

Input Voltage

+5V

Steady State Power Consumption

≤5W

External Dimension

50mmx50mmx37.5mm

Weight

≤145g

Note: All performance parameters and interfaces are customizable to mission requirements.

 








MECHANICAL  AND  OPTICAL  INTERFACE  DIAGRAM











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