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TECHNOLOGICAL INNOVATION，NAVIGATING THE FUTURE
1 Years
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| Brand Name : | Liocrebif |
| Model Number : | LKF-F3X100 |
| Certification : | GJB 9001C-2017 |
| Price : | 5000-25000CHY |
| Payment Terms : | T/T |
| Supply Ability : | 10000 |
| Delivery Time : | 2-4 weeks |
Introduction
Fiber optic gyro, as a new type of all-solid-state gyro, has the advantages of fast startup, wide measurement range and high reliability. Among them, LKF-F3X100-IMU type fiber optic gyro inertia set is designed for the needs of medium and low precision application background, adopting three-axis shared technology design, low cost and stable performance; the structure adopts the integrated package of optical circuit and circuit, simple structure, easy installation, and it can be applied in the system of navigation and guidance, attitude measurement and control of small missiles, guided bombs, and so on.
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.
Aerospace Applications In aerospace applications, high-precision interferometric fiber optic gyroscopes are generally used. The LKF-F3X100-IMU fiber optic gyro inertial unit can provide the aircraft with three-dimensional angular velocity, position, angle of attack and sideslip angle to achieve tracking and measurement of rocket launches.
Fiber Optic Gyroscope | Index | |
Type | H | M |
Bias Repeatability at Room Temperature (By times, by days) (º/h) | ≤0.05 | ≤0.1 |
Bias stability at Constant Temperature (º/ h) | ≤0.05 | ≤0.1 |
Scale Factor Repeatability at Room Temperature (ppm) | ≤20 | ≤20 |
Scale Factor Asymmetry at Constant Temperature (ppm) | ≤20 | ≤20 |
Scale Factor Nonlinearity at Constant Temperature (ppm) | ≤30 | ≤30 |
Threshold (º/h) | ≤0.1 º/h | |
Angular Rate Range (º/s) | -500 to +500 º/s | |
Bandwidth (Hz) | ≥200 | |
Dimensions (mm) | 100*100*95 | |
Weight (g) | 1100±50 (with accelerometer) | |
Operating Temperature (°C) | -45 to +65 | |
Quartz Accelerometer | ||
No | Item | Technical Requirement |
1 | Range (g) | ≥±30 |
2 | Scale Factor Temperature Coefficient (ppm /°C) | ≤60 |
3 | Scale Factor Monthly Stability (ppm) | ≤60 |
4 | Bias (mg) | ≤±7 |
5 | Bias Temperature Coefficient (μg /°C) | ≤60 |
6 | Bias Monthly Stability (μg) | ≤60 |
7 | Second-order Nonlinear Coefficient (μg /g2) | ≤60 |
8 | Mounting angle (") | ≤200 |
9 | Outlook | No scratch, crack, corrosion |
Table 2 The electrical interface of the gyroscope uses J30-15ZK connector
LKF-F3X100-IMU/INS Output Definition | ||
J30J-15ZK | Define | Note |
5, 13 | +24V | Inertia Combination Power Supply |
6, 7 | +24V (ground) | |
1 | T3+ | Serial Port |
2 | T3- | |
3 | R3+ | |
4 | R3- | |
11 | T2+ | IMU Data Output Serial Port |
12 | T2- | |
14 | T1+ | Debugging Serial Ports |
15 | T1- | |
9 | R1+ | |
10 | R1- | |
Main Features
High Degree of Engineering, Highly Cost-Effective
Pure Solid-State Design with Strong Environmental Adaptability
Full Digital RS-422 Electrical Interface Output
Application
Navigation guidance
Attitude measurement and control systems for small missiles and guided bombs
Fig. 1 Dimensions of the external structure
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