Single Axis Interferometric Fiber Optic Gyroscope Compact For Navigation
Brand Name:Liocrebif
Certification:GJB 9001C-2017
Model Number:LKF-FS50X
Minimum Order Quantity:1
Delivery Time:2-4 weeks
Payment Terms:T/T
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Location:
Wuhan Hubei China
Address:
No. 17, Jiangxia Avenue, Jiangxia District Wuhan City, Hubei Province
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within 25 hours
Product Details
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Product Details
Essential details
MOQ:1
Size:L(5)*W(5)*H(3.65) cm
Specification Number:LKF-FS50X
Product Introduction
Introduction
LKF-FS50X is a miniaturized closed-loop fiber optic gyroscope, which breaks through the classical design concept of traditional fiber optic gyroscope. It adopts integrated circuit and optical path design. It has the outstanding characteristics of small volume, light weight, high bandwidth, fast start-up, simple interface and convenient use. LKF-FS50X is an ideal medium-low precision angular rate sensor in the control field, which is widely used in various inertial measurement and control fields.
By reducing the outer diameter of fiber to 135μm,Thin PM fiber solution decreases extremely the size of fiber coils and delivers outstanding precision performance in fiber coils, which is applied for miniaturization of FOGs. And, the coils are wound precisely through quadrupole symmetry method.
By using inertial devices and strapdown inertial navigation technology, accurate speed, position and attitude information can be provided for the UAV, thereby achieving precise navigation, positioning and attitude control. LKF-FS50X can greatly improve the performance of inertial navigation and is an ideal choice for medium-low precision inertial navigation.
Table 1 Performance parameters of LKF-FS50A single-axis FOG | |||
A | B | C | |
Bias Stability °/hr(1σ,10s) | ≤0.30 | ≤0.20 | ≤0.10 |
Stabilization Time S | <10 | <10 | <10 |
Bias Repeatability °/hr(1σ) | ≤0.30 | ≤0.20 | ≤0.10 |
Full Temperature Bias Repeatability °/hr | ≤1 | ≤0.5 | ≤0.3 |
Random Walk Coefficient °/ | ≤0.02 | ≤0.02 | ≤0.01 |
Scale Factor Nonlinearity ppm(1σ) | ≤100 | ≤50 | ≤50 |
Scale Factor Repeatability ppm(1σ) | ≤100 | ≤50 | ≤50 |
Dynamic Range | ±500°/s | ||
Magnetic Field Sensitivity | ≤0.10°/hr/Gs | ||
Operating Temperature | -40℃～+70℃ | ||
Storage Temperature | -50℃～+70℃ | ||
Vibration Condition | 4.2g,20Hz～2000Hz | ||
Table 2 Performance parameters of LKF-FS50X single-axis FOG | |||
A | B | C | |
Bias Stability °/hr(1σ,10s) | ≤0.20 | ≤0.10 | ≤0.05 |
Stabilization Time S | <10 | <10 | <10 |
Bias Repeatability °/hr(1σ) | ≤0.30 | ≤0.20 | ≤0.10 |
Full Temperature Bias Repeatability °/hr | ≤0.6 | ≤0.4 | ≤0.3 |
Random Walk Coefficient °/ | ≤0.02 | ≤0.02 | ≤0.01 |
Scale Factor Nonlinearity ppm(1σ) | ≤50 | ≤30 | ≤20 |
Scale Factor Repeatability ppm(1σ) | ≤50 | ≤30 | ≤30 |
Dynamic Range | ±500°/s | ||
Magnetic Field Sensitivity | ≤0.05°/hr/Gs | ||
Operating Temperature | -40℃～+70℃ | ||
Storage Temperature | -50℃～+70℃ | ||
Vibration Condition | 4.2g,20Hz～2000Hz | ||
Main Features
Miniature and compact design
Pure solid shell design
Environment Edaptive
High Reliability and Long Life
Fully Digital RS-422 Electrical Output
Application
Electro-optical Pod
Flight Control Platform
Optical/Photographic Platform
Platform Stabilizer
Satcom on the Move
Inertial Measurement Unit
Light UAV
Fig. 1 Dimensions of the external structure FS50A
Fig. 2 Dimensions of the external structure FS50X
Single Axis Interferometric Fiber Optic Gyroscope Compact For Navigation
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