| MOQ: | 1 set |
| Price: | $1000-$100000 |
| Delivery Period: | 30 work days |
| Payment Method: | T/T |
| Supply Capacity: | 1000 sets per year |
RLG (Dubhe-90)
The Ring Laser Gyroscope (RLG) operates based on the Sagnac effect, measuring angular increments by detecting the phase difference between counter-propagating laser beams within a closed glass cavity.
With high integration, exceptional reliability, strong environmental adaptability, and stable performance, the Dubhe-90 RLG is widely used in high-precision inertial navigation systems (INS).
The Dubhe-90 RLG is suitable for navigation and attitude reference in:
Spacecraft
Aircraft
Satellites
Vehicles
Ships
Submersibles
Monolithic optical and electronic packaging, enabling easy installation
Compact and lightweight design with controlled power consumption
High reliability with strong resistance to shock and vibration
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 | |
| MOQ: | 1 set |
| Price: | $1000-$100000 |
| Delivery Period: | 30 work days |
| Payment Method: | T/T |
| Supply Capacity: | 1000 sets per year |
RLG (Dubhe-90)
The Ring Laser Gyroscope (RLG) operates based on the Sagnac effect, measuring angular increments by detecting the phase difference between counter-propagating laser beams within a closed glass cavity.
With high integration, exceptional reliability, strong environmental adaptability, and stable performance, the Dubhe-90 RLG is widely used in high-precision inertial navigation systems (INS).
The Dubhe-90 RLG is suitable for navigation and attitude reference in:
Spacecraft
Aircraft
Satellites
Vehicles
Ships
Submersibles
Monolithic optical and electronic packaging, enabling easy installation
Compact and lightweight design with controlled power consumption
High reliability with strong resistance to shock and vibration
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 | |