|
| الـ MOQ: | 1 مجموعة |
| السعر: | $1000-$100000 |
| فترة التسليم: | 30 يوم عمل |
| قدرة التوريد: | 1000 مجموعة في السنة |
RLG(Dubhe-90)
The Ring Laser Gyroscope (RLG) operates on the Sagnac effect principle, measuring angular increments by detecting phase differences of laser beams in a closed glass cavity. Featuring high integration, exceptional reliability, strong environmental adaptability and stable performance, it has become the sensor of choice for high-precision inertial navigation systems worldwide. Applications include spacecraft, aircraft, satellites, vehicles, ships and submersibles for navigation and attitude reference.
Key features: 1) Monolithic optical/electronic packaging for easy installation; 2) Compact, lightweight design with controlled power consumption; 3) High reliability and shock/vibration resistance; 4) Wide dynamic response bandwidth with digital output.
| Series | RLG Series | |
| Type | Dubhe-90 | |
| Performance | Bias stability (1σ) | 0.004°/h~0.002°/h |
| Zero bias repeatability (1σ) | 0.002°/h~0.001°/h | |
| ARW(Angular random walk(1σ) | 0.0007°/√hr~0.0004°/√hr | |
| Scale factor error (1σ) | ≤2ppm | |
| Dynamic Range | ≥±400°/s | |
| Bandwidth | ＞200Hz | |
| Electrical Interface | Turn on time | ＜5s |
| Output signal format | TTL | |
| Built in self-test | yes | |
| Output signal update rate | 1Hz | |
| Output signal baud rate | 115200 | |
| Vibration shock | 75g, half sine, 6ms | |
| Operating temperature | - 40℃ ~ + 70℃ | |
| Storage temperature | - 55℃ ~ + 85℃ | |
| Physical Specifications | Power supply | ±15V,±5V |
| Connector (25 pins) | J30JM-37ZKP36 | |
| Power consumption | ≤3W | |
| MTBF (per MIL-HDBK-217-F) | ＞10000hr | |
| Weight | 2kg | |
| Dimensions | 151mm×126mm×57mm | |
|
|
| الـ MOQ: | 1 مجموعة |
| السعر: | $1000-$100000 |
| فترة التسليم: | 30 يوم عمل |
| قدرة التوريد: | 1000 مجموعة في السنة |
RLG(Dubhe-90)
The Ring Laser Gyroscope (RLG) operates on the Sagnac effect principle, measuring angular increments by detecting phase differences of laser beams in a closed glass cavity. Featuring high integration, exceptional reliability, strong environmental adaptability and stable performance, it has become the sensor of choice for high-precision inertial navigation systems worldwide. Applications include spacecraft, aircraft, satellites, vehicles, ships and submersibles for navigation and attitude reference.
Key features: 1) Monolithic optical/electronic packaging for easy installation; 2) Compact, lightweight design with controlled power consumption; 3) High reliability and shock/vibration resistance; 4) Wide dynamic response bandwidth with digital output.
| Series | RLG Series | |
| Type | Dubhe-90 | |
| Performance | Bias stability (1σ) | 0.004°/h~0.002°/h |
| Zero bias repeatability (1σ) | 0.002°/h~0.001°/h | |
| ARW(Angular random walk(1σ) | 0.0007°/√hr~0.0004°/√hr | |
| Scale factor error (1σ) | ≤2ppm | |
| Dynamic Range | ≥±400°/s | |
| Bandwidth | ＞200Hz | |
| Electrical Interface | Turn on time | ＜5s |
| Output signal format | TTL | |
| Built in self-test | yes | |
| Output signal update rate | 1Hz | |
| Output signal baud rate | 115200 | |
| Vibration shock | 75g, half sine, 6ms | |
| Operating temperature | - 40℃ ~ + 70℃ | |
| Storage temperature | - 55℃ ~ + 85℃ | |
| Physical Specifications | Power supply | ±15V,±5V |
| Connector (25 pins) | J30JM-37ZKP36 | |
| Power consumption | ≤3W | |
| MTBF (per MIL-HDBK-217-F) | ＞10000hr | |
| Weight | 2kg | |
| Dimensions | 151mm×126mm×57mm | |
