Fiber optic gyroscopes for aircraft navigation and platform stability testing with ≤0.01(°) / H Bias drift
Brand Name:Kacise
Certification:certificate of explosion-proof, CE
Model Number:KSFG-98
Minimum Order Quantity:1pcs
Delivery Time:5-8 working days
Payment Terms:T/T, Western Union, MoneyGram
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Address:
i City, No11, TangYan South road, Yanta District, Xi'an,Shaanxi,China.
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Product Details
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Product Details
Product Description:
The Electronic Gyroscope Sensor is a compact and reliable fiber
optic gyroscope with high accuracy and stability. It features
excellent dynamic range, low power consumption, wide-operating
temperature range and low cost. It is a perfect choice for
applications involving precision navigation, attitude measurement,
and motion control.
Functioning as an inertial angle rate sensor, this product relies
on the optical Sagnac effect to measure the rotational angular
velocity along the sensitive axis of the carrier. A digital
closed-loop detection circuit is employed for extracting the
optical path difference in clockwise light induced by external
physical angular speed. The voltage signal of the optical path
undergoes modulation and demodulation, enabling closed-loop
feedback and control for real-time detection of angular velocity
signals.
Constituents and Objectives: Comprising two essential components—an optical angular velocity sensitive unit and a signal detection apparatus—the product provides crucial information on uniaxial angle increments and internal temperature.
Application Scope: Specifically designed for implementation in photoelectric cranes, conventional cranes, flying platforms, inertial navigation systems, inertial measurement systems, optical instruments, photographic devices, platform stabilization equipment, and inertial measurement instruments.
Technical Parameters:
| Sn# | Test item | H | L | Remark |
| 1 | Dimensions (mm) | 98×98×35 | 98×98×35 | |
| 2 | start time (s) | ≤5 | ≤5 | |
| 3 | Bias drift (°) / h (10s smooth, fix temperature) | ≤0.015 | ≤0.03 | |
| 4 | Bias drift (°) / h (10s smooth) -45~ + 70 | ≤0.03 | ≤0.06 | |
| 5 | Bias repeatability (°) / h | ≤0.005 | ≤0.01 | |
| 6 | Random walk coefficient(º)/h1/2 | ≤0.001 | ≤0.002 | |
| 7 | Scale factor non-linearity (ppm) | ≤10 | ≤20 | |
| 8 | Scale factor repeatability (ppm) | ≤10 | ≤20 | |
| 9 | Operate temperature ℃ | -40～+70 | -40～+70 | |
| 10 | Storage temperature of (℃) | -45～+80 | -45～+80 | |
| 11 | Dynamic range (°) / s | ±300 | ±300 | |
| 12 | Supply voltage (V) | ±5 | ±5 | |
| 13 | Steady-state power consumption (full temperature) (W) | <3 | <3 | |
| 14 | weight (g) | ＜550 | ＜550 |
Support and Services:
We provide technical support and services for our Electronic Gyroscope Sensor. Our technical support team is available 24 hours a day, 7 days a week to assist you with any questions or issues you may have. We also provide a warranty for our products, ensuring that you can purchase with confidence.
Our customer service team is always available to help with any additional questions or concerns you may have regarding our Electronic Gyroscope Sensor. We strive to provide the best customer service experience possible, and will do our best to ensure you are satisfied with your purchase.
For any additional information on our Electronic Gyroscope Sensor, please feel free to contact us directly. We look forward to hearing from you!
Packing and Shipping:
Packaging and Shipping: Electronic Gyroscope Sensor
The Electronic Gyroscope Sensor is securely packaged in a foam-lined box for maximum protection during shipping. It is then placed in a sturdy cardboard shipping box with additional packaging material for extra cushioning. The box is sealed and labeled with the product name and shipping address.
The package is then shipped via a reliable courier service such as FedEx, UPS, or DHL. Tracking information will be provided to the customer so that they can easily monitor the progress of the shipment.
Fiber optic gyroscopes for aircraft navigation and platform stability testing with ≤0.01(°) / H Bias drift
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