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Fiber Optic Gyro
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Small Size Close-Loop Fiber Optic Gyroscope Zero Bias Stability 0.2~0.8°/

Small Size Close-Loop Fiber Optic Gyroscope Zero Bias Stability 0.2~0.8°/

Brand Name: Firepower
Model Number: F60A
MOQ: 1 pcs
Price: US$2,500.00-3,500.00
Payment Terms: L/C, T/T
Supply Ability: 500 pcs per month
Detail Information
Place of Origin:
Shenzhen, China
Certification:
CE
Measuring Rsnge:
±400~±800(optional)
Zero Bias Stability:
≤ 0.05°/h, 10s
Zero Bias Repeatability:
≤ 0.05°/h
Random Walk Coefficient:
≤0.006º/√h
Scale Factor Nonlinearity:
≤50ppm
Scale Factor Repeatability:
≤50ppm
Scale Factor Asymmetry:
≤50ppm
Start Time:
≤1s
Bandwidth:
500Hz
Power Supply:
±5±0.15V
Power:
≤6W
Operating Temperature:
-40~+70°C
Storage Temperature:
-55~+85°C
Vibration:
20~2000Hz, 0.06g²/Hz
Impact:
30g, 11ms
Baud Rate:
921600(Customizable)bps
Output Mode:
RS-422
Connector:
J30J-15TJL/(Customizable)
Overall Dimensions:
60mm*60mm*32mm
Installation Dimensions:
52mm*52mm
Packaging Details:
Sponge and box
Supply Ability:
500 pcs per month
Highlight:

Small Size Fiber Optic Gyroscope

,

Close-Loop Fiber Optic Gyroscope

Product Description

Basic Info.

Model NO.
F60
Measuring Shaft Quantities
Single
Accuracy Grade
≤0.05°/H
IP Rating
IP67
Certification
CE
Customized
Customized
Non-Linearity Scale Factor
<50ppm (1sigma;)
Scale Factor Asymmetry
<50ppm
Scale Factor Repeatability
<50ppm
Dynamic Range
300 Deg;/S
Zero Bias Stability
<0.05 Deg;/H (1sigma;)
Bandwidth
>200Hz
Transport Package
Sponge and Box
Specification
70mm× 70mm× 32mm
HS Code
9031809090
Production Capacity
500/Month

Product Description

Single Axis Optical Sagnac Effect GyroInertial Angular Rate Fog Gyroscope

This document specifies the requirements and methods for the use and maintenance of FOG-60 fiber optic gyroscope (product for short).
Product introduction
1 Working principle, function and scope of application of the produc
1.1 How it works This product is an inertial angular rate sensor based on the optical Sagnac effect, which is used to measure the angular rate of the carrier along the sensitive axis of the product. The angular rate sensing unit of the product is an optical fiber ring, and a digital closed-loop detection circuit is adopted to extract the optical path difference of clockwise and anticlockwise propagating light caused by the external physical angular rate, which is sensed by the optical fiber ring,At the same time, the voltage signal converted from the optical path difference signal is used for closed-loop feedback and control to realize the modulation and demodulation of the signal and achieve the purpose of angular velocity signal detection.
1.2 Function This product is composed of an optical angular velocity sensing unit and a signal detection unit, providing single-axis angular increment information and internal temperature information.
1.3 Scope of application The products are mainly suitable for applications such as medium-precision inertial navigation systems, positioning and orientation systems, and servo stabilization systems.
2 Composition The main components of the product are as follows: a) The optical path unit comprise an SLD light source, an optical fiber re, an integrated optical phase modulator, an optical fiber coupler and an optical detector; b) The circuit unit comprises a light source driving circuit and a detection and control signal circuit board; c) Gyroscope structural parts.
3 Appearance and installation dimension Overall dimension (mm): (60 ± 0.1) × (60 ± 0.1) × (31 ± 0.1) (L × W × H); Installation dimension (mm): (50 ± 0.1) × (50 ± 0.1) (L × W), Φ3.2mm × 4,
such asFigure 1 As shown.


Single Axis Optical Sagnac Effect Gyroinertial Angular Rate Fog Gyroscope
Main performance
parameters See the main performance parameters of the product for details.
Table 1 Main performance parameters
Serial number Test item Unit Technical requirements
1 Overall dimensions mm 60×60×31
2 Start time s 5
3 Zero bias stability
(10 s smoothing, 1σ)
º/h ≤0.1
4 Zero-bias repeatability º/h ≤0.1
5 Random walk coefficient º/h1/2 ≤0.01
6 Scale factor nonlinearity ppm ≤50
7 Scale factor repeatability ppm ≤50
8 Operating temperature ºC -40~+700
9 Storage temperature ºC -50~+70
10 Dynamic range (°)/s ±1000
11 Supply voltage V +5
12 Steady-state power consumption W <4


Power requirements
Serial number Name Request
1 Power supply accuracy ±5%
2 Power ripple (Vpp) 20mV
3 Supply current >1.5A

Electrical connection interface
Core point number Definition Comment
1 +5V Power supply input
2 GND Power ground
3 -- Reserved
4 RXD+ Gyro differential sorting and correcting
5 TXD+ Gyro RS422 output positive
6 +5V Power supply input
7 GND Power ground
8 RXD- Gyro differential gating negative
9 TXD- Gyro RS422 output negative
 

About company

 

Small Size Close-Loop Fiber Optic Gyroscope Zero Bias Stability 0.2~0.8°/ 1

Factory Photos
Single-Axis Rotary Test Turntable For Aerospace And Defense Calibration 2
Single-Axis Rotary Test Turntable For Aerospace And Defense Calibration 3
Single-Axis Rotary Test Turntable For Aerospace And Defense Calibration 4
Single-Axis Rotary Test Turntable For Aerospace And Defense Calibration 5
Single-Axis Rotary Test Turntable For Aerospace And Defense Calibration 6
Single-Axis Rotary Test Turntable For Aerospace And Defense Calibration 7
Single-Axis Rotary Test Turntable For Aerospace And Defense Calibration 8
Single-Axis Rotary Test Turntable For Aerospace And Defense Calibration 9
Main Applications
Single-Axis Rotary Test Turntable For Aerospace And Defense Calibration 10
Single-Axis Rotary Test Turntable For Aerospace And Defense Calibration 11
Single-Axis Rotary Test Turntable For Aerospace And Defense Calibration 12

Small Size Close-Loop Fiber Optic Gyroscope Zero Bias Stability 0.2~0.8°/ 13

Small Size Close-Loop Fiber Optic Gyroscope Zero Bias Stability 0.2~0.8°/ 14

Small Size Close-Loop Fiber Optic Gyroscope Zero Bias Stability 0.2~0.8°/ 15

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