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Aero-grade FOG sensor for aircraft navigation system with ≤0.03(°/h) Bias repeatability and ≤0.005(º/h1/2) Random walk

Aero-grade FOG sensor for aircraft navigation system with ≤0.03(°/h) Bias repeatability and ≤0.005(º/h1/2) Random walk

  • Aero-grade FOG sensor for aircraft navigation system with ≤0.03(°/h) Bias repeatability and ≤0.005(º/h1/2) Random walk
  • Aero-grade FOG sensor for aircraft navigation system with ≤0.03(°/h) Bias repeatability and ≤0.005(º/h1/2) Random walk
  • Aero-grade FOG sensor for aircraft navigation system with ≤0.03(°/h) Bias repeatability and ≤0.005(º/h1/2) Random walk
Aero-grade FOG sensor for aircraft navigation system with ≤0.03(°/h) Bias repeatability and ≤0.005(º/h1/2) Random walk
Product Details:
Place of Origin: China (Mainland)
Brand Name: Kacise
Certification: certificate of explosion-proof, CE
Model Number: KSFG-70
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
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Detailed Product Description
Bias Repeatability: ≤0.03(°/h) Random Walk: ≤0.005(º/h1/2)
Dynamic Range: ±500(°/s) Bias Drift (10s Smooth, Fix Temperature): ≤0.03(°/h)
Supply Voltage: +5(V) Operate Temperature: -40~+70(℃)
Start Time: 5(s) Bias Drift (10s Smooth) -45~ + 70℃: ≤0.1(°/h)
High Light:

Aero-grade FOG sensor

,

FOG sensor for aircraft navigation system

,

aircraft navigation system FOG sensor

Product Description:

Product Description

The inertial angle rate sensor we offer employs the optical Sagnac effect as the fundamental principle to measure the rotational angular velocity along its sensitive axis. The essence of this product lies in its capability to sense the rotation of the carrier on which it is mounted. Utilizing the cutting-edge closed-loop detection circuitry, the sensor accurately determines the clockwise light's optical path difference. This discrepancy is a direct result of the external angular velocity imposed on the sensor.

Moreover, the sensor system adeptly handles the modification and demodulation of the voltage signal derived from the optical path. Strategically integrated into the device is a closed loop feedback mechanism, which facilitates precise control. This advanced functionality empowers the sensor to conduct real-time detection of angular velocity signals, ensuring the fidelity and reliability of the readings.

Functional Components

Our product is architecturally divided into two core components. The first is the optical angular velocity sensitive unit; this unit is the heart of the sensor, responsible for capturing the angular movements with sensitivity and precision. The second is the signal detection mechanism, which processes the raw data obtained from the sensitive unit.

Together, these two components work in harmony to provide users with valuable information. The sensor not only offers uniaxial angle increment data but also integrates internal temperature readings. These dual capabilities make our sensor not only a robust tool for monitoring rotational movements but also an intelligent device aware of its operational environment.

 

Features:

  • Product Name: Electronic Gyroscope Sensor
  • Weight (g): <290
  • Dimensions (mm): 70×70×32
  • Storage temperature (℃): -45~+80
  • Start time (s): 5
  • Scale factor non-linearity (ppm): ≤10
  • Technology: Fiber optic gyro
  • Type: Gyroscope
  • Application: Airplane gyroscope
 

Technical Parameters:

Sn# test item H M L
1 Dimensions (mm) 70×70×32 70×70×32 70×70×32
2 start time (s) 5 5 5
3 Bias drift (°) / h (10s and 100s smoothing, fix temperature)

≤0.03(10s)

≤0.01(100s)

≤0.05 ≤0.3
4 Bias drift (°) / h (10s smoothing) -45~ + 70℃ ≤0.1 ≤0.15 ≤0.5
5 Bias repeatability (°) / h ≤0.03 ≤0.05 ≤0.3
6 Random walk coefficient(º)/h1/2 ≤0.005 ≤0.01 ≤0.02
7 Scale factor non-linearity (ppm) ≤10 ≤20 ≤50
8 Scale factor repeatability (ppm) ≤10 ≤20 ≤50
9 Operate temperature (℃) -40~+70 -40~+70 -40~+70
10 Storage temperature of (℃) -45~+80 -45~+80 -45~+80
11 Dynamic range (°) / s ±500 ±500 ±500
12 Supply voltage (V) ±5 ±5 ±5
13 Steady-state power consumption (full temperature) (W) <4 <4 <4
14 weight (g) <290 <290 <290
 

Product Description:

Introduction to the Inertial Angle Rate Sensor

Our cutting-edge product is an inertial angle rate sensor that operates on the principles of the optical Sagnac effect . It is designed primarily to measure the rotational angular velocity of various carriers. The measurements are taken along the axis that is sensitive to the sensor's orientation.

Technical Mechanism

The core functionality involves a digital closed-loop detection circuit . This sophisticated circuitry actively extracts the difference in optical path length of the clockwise light. The differentiation is brought about as a result of the carrier's physical angular velocity. Consequent to this, the voltage signal associated with the optical path is carefully modulated and demodulated.

Furthermore, a robust system of closed-loop feedback and control is implemented within the device. This system is crucial for accomplishing the goal of real-time angular velocity signal detection , thereby offering reliable and accurate performance in dynamic environments.

Features and Utility

The sensor is composed of two interconnected parts. One is the optical angular velocity sensitive unit , and the other is the signal detection module . Together, they provide valuable data. The sensor is capable of delivering precise information regarding the uniaxial angle increment . Additionally, it monitors and reports on the internal temperature of the device, which can be crucial for specific operational conditions.

 

Features:

  • Product Name: Electronic Gyroscope Sensor
  • Weight (g): <290
  • Scale factor repeatability (ppm): ≤10
  • Dynamic range (°) / s: ±500
  • Steady-state power consumption (full temperature) (W): <4
  • Bias drift (°) / h (10s smooth, fix temperature): ≤0.03
  • Technology: fiber optic gyro
  • Type: gyro
  • Design: fiber optic gyroscope
 

Technical Parameters:

Sn# test item H M L
1 Dimensions (mm) 70×70×32 70×70×32 70×70×32
2 start time (s) 5 5 5
3 Bias drift (°) / h (10s and 100s smoothing, fix temperature)

≤0.03(10s)

≤0.01(100s)

≤0.05 ≤0.3
4 Bias drift (°) / h (10s smoothing) -45~ + 70℃ ≤0.1 ≤0.15 ≤0.5
5 Bias repeatability (°) / h ≤0.03 ≤0.05 ≤0.3
6 Random walk coefficient(º)/h1/2 ≤0.005 ≤0.01 ≤0.02
7 Scale factor non-linearity (ppm) ≤10 ≤20 ≤50
8 Scale factor repeatability (ppm) ≤10 ≤20 ≤50
9 Operate temperature (℃) -40~+70 -40~+70 -40~+70
10 Storage temperature of (℃) -45~+80 -45~+80 -45~+80
11 Dynamic range (°) / s ±500 ±500 ±500
12 Supply voltage (V) ±5 ±5 ±5
13 Steady-state power consumption (full temperature) (W) <4 <4 <4
14 weight (g) <290 <290 <290

 

Dimensions:

Aero-grade FOG sensor for aircraft navigation system with ≤0.03(°/h) Bias repeatability and ≤0.005(º/h1/2) Random walk 0Aero-grade FOG sensor for aircraft navigation system with ≤0.03(°/h) Bias repeatability and ≤0.005(º/h1/2) Random walk 1

Applications:

Product Application Scope

Our range of products is engineered to serve a variety of uses. They are primarily designed to accommodate the needs of the following areas:

  • Photoelectric Cranes: Perfect for integrating with crane systems that utilize photoelectric technology for enhanced precision and control.
  • Crane Applications: Ideal for various kinds of crane operations requiring reliable and high-performance components.
  • Flying Platforms: Compatible with aerial work platforms, helping to maintain stability and control at elevated heights.

In addition, our products find their applications in the following sectors:

  • Inertial Navigation Systems: These systems, critical for determining orientation and position, benefit greatly from our products' accuracy and reliability.
  • Inertial Measurement Systems: Our products enhance the capability of systems that measure velocity, orientation, and gravitational forces.
  • Optical and Photographic Instruments: The precision of our product line contributes to the performance of devices in photography and optics.
  • Platform Stabilization Devices: Essential for systems requiring stability, our products provide the necessary support for steady performance.
  • Inertial Measurement Instruments: Our offerings are integral components of instruments used for detecting and measuring motion, acceleration, and rotation.
 

Support and Services:

Welcome to the Product Technical Support and Services for our Electronic Gyroscope Sensor. Our dedicated team is committed to providing you with comprehensive support and services to ensure the optimal performance of your gyroscope sensor. We offer a range of technical support services to meet your needs.

If you're experiencing issues with your Electronic Gyroscope Sensor, we provide troubleshooting assistance to help diagnose and resolve common problems. Our step-by-step guides and detailed support articles are designed to help you understand your sensor's functionality and address any concerns you may have.

For those who require more in-depth technical assistance, our expert support team is available to provide personalized guidance. We can help with advanced configuration, integration with other devices, and optimization of your sensor for specific applications. Our goal is to ensure that your sensor is functioning at its best.

In addition to troubleshooting and technical assistance, we offer firmware updates to keep your Electronic Gyroscope Sensor up-to-date with the latest features and improvements. Regular updates can enhance sensor performance, introduce new functionalities, and improve overall reliability.

We also provide a comprehensive FAQ section that covers a wide range of topics related to the Electronic Gyroscope Sensor. This resource is designed to provide quick answers to common questions and help you get the most out of your device.

Your satisfaction is our top priority. We strive to deliver the highest quality support and services to our customers. If you have any further questions or require additional assistance, please feel free to reach out to our support team (excluding contact information).

 

Packing and Shipping:

Product Packaging:

The Electronic Gyroscope Sensor is meticulously packed in an anti-static bag to prevent electrostatic discharge damage. It is then cushioned with foam inserts to secure and stabilize the device within a sturdy, compact cardboard box. Each box is clearly labeled with product information and handling instructions to ensure the safety and integrity of the sensor during transport.

Shipping:

Our Electronic Gyroscope Sensor is shipped with a trusted courier for fast and reliable delivery. The package is tracked and insured, with the tracking number provided to the customer immediately after dispatch. We take every precaution to ensure that the product reaches you in perfect working condition. Please inspect the package upon arrival and report any damage within 48 hours for prompt resolution.

 

Contact Details
Xi'an Kacise Optronics Co.,Ltd.

Contact Person: Ms. Evelyn Wang

Tel: +86 17719566736

Fax: 86--17719566736

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Contact

Address: i City, No11, TangYan South road, Yanta District, Xi'an,Shaanxi,China.

Factory Address:i City, No11, TangYan South road, Yanta District, Xi'an,Shaanxi,China.