TG-40 three-axis fiber optic gyroscope
extremely low power consumption, all-temperature performance, Excellent environmental adaptability, strong impact and vibration resistance
TG-40 three-axis integrated fiber optic gyroscope
| Indicators |
Model |
TG-40 |
| Performance indicators |
bias stability① (°/h, 1σ) |
0.1 |
| bias stability② (°/h, 1σ) |
0.05 |
| bias stability③ (°/h,1σ) |
0.5 |
| bias repeatability(°/h, 1σ) |
0.1 |
| random walk(°/h 1/2) |
0.01 |
| scale factor nonlinearity(ppm) |
20 |
| scale factor asymmetry(ppm) |
10 |
|
scale factor repeatability
(ppm)
|
20 |
| dynamic range(°/s) |
±500 |
|
Mechanical/
electrical interface
|
size(mm) |
70×66×45 |
| weight(g) |
350±10 |
| steady state power consumption at normal temperature(W) |
4 |
| power supply(V) |
+5 |
| communication interface |
RS422 |
|
remarks:
① Static test at room temperature, 10s smooth, 1σ;
② Static test at room temperature, smooth for 100s, 1σ;
③ The temperature change rate is 1℃/min, smooth for 100s, 1σ.
|
◾ Product introduction
TG-40 three-axis integrated fiber optic gyroscope is a full solid-state high-precision digital closed-loop fiber optic gyroscope integrating optics, mechanics and electricity. Based on the principle of Sagnac, it is composed of SLD light source, fiber coupler, photodetector, integrated optical phase modulator, fiber sensing ring, circuit and structure.
It is specially designed for miniaturized inertial measurement systems, and has the characteristics of small size, high precision, high reliability, and flexible structure. The installation position of quartz accelerometer or MEMS accelerometer is included, and it can be produced according to the platform designed by customers.
TG-40 is the best choice for small inertial measurement systems!
◾ Product features
• Single 5V power supply, extremely low power consumption
• Excellent all-temperature performance
• Excellent start-up performance, the nominal index can be reached when the power is turned on, and no preheating is required
• Excellent environmental adaptability, strong impact and vibration resistance
• Interference fringe recognition technology, supporting full dynamic range cold start
• High reliability
• No dead zone
◾ Typical applications
• Miniaturized missile-borne inertial navigation system
• Attitude indicator
• Small compass
◾Performance indicators
• Turn-on time (s) 3
• Dynamic range (°/s) ±500
• Zero position (°/h ) ≤1
• Bias stability① (°/h , 1σ) ≤0.1
• Bias stability② (°/h , 1σ) ≤0.05
• Bias stability③ (°/h , 1σ) ≤0.5
• Bias repeatability (°/h , 1σ) ≤0.1
• Bias magnetic sensitivity (°/h/Gs) ≤0.1
• Random walk (°/h 1/2) ≤0.01
• Scale factor nonlinearity (ppm) ≤50
• Scale factor asymmetry (ppm) ≤10
• Scale factor repeatability (ppm) ≤20
• Threshold (°/h ) ≤0.1
• Resolution (°/h ) ≤0.1
• Bandwidth (Hz) ≥200
◾Physical/Electrical
• Power supply +5V
• Steady-state power consumption ≤3W
• Steady-state power consumption at full temperature ≤4W
• Instantaneous power consumption at startup ≤4W
• Dimensions 70㎜×66㎜×45㎜
• Weight 350g±10g
• Electrical form RS422
◾Environmental adaptability
• Operating temperature -45℃ - +70℃
• Storage temperature -55℃ - +80℃
• Vibration 6.06g (RMS), 20Hz-2000Hz
• Impact 30g, 6ms-8ms
• Average trouble-free time 8000h
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