| MOQ: | 1 set |
| Price: | $1000-$100000 |
| Delivery Period: | 30 work days |
| Payment Method: | T/T |
| Supply Capacity: | 1000 sets per year |
The Dubhe-90 Ring Laser Gyroscope (RLG) is a high-performance inertial sensor based on the Sagnac effect, designed for high-precision inertial navigation systems (INS). It measures angular increments by detecting the phase difference between counter-propagating laser beams within a closed monolithic glass cavity, delivering accurate and stable angular rate information.
With high integration, excellent long-term stability, and strong environmental adaptability, the Dubhe-90 RLG has become a preferred solution for space-grade and high-end navigation applications worldwide.
The Dubhe-90 Ring Laser Gyroscope is widely used in:
Spacecraft and launch vehicles
Aircraft and UAV inertial navigation systems
Satellites and space platforms
Land vehicles and autonomous systems
Marine vessels and submarines
High-precision attitude and heading reference systems (AHRS)
Monolithic optical and electronic integration, enabling easy installation and high system reliability
Compact and lightweight design with optimized and controlled power consumption
High reliability with strong resistance to shock and vibration, suitable for harsh environments
Wide dynamic response bandwidth with high-resolution digital output, supporting real-time navigation and control
The Dubhe-90 RLG provides ultra-low bias drift, stable performance, and long operational life, making it an ideal core sensor for advanced INS, navigation, and attitude reference systems.
| 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 |
The Dubhe-90 Ring Laser Gyroscope (RLG) is a high-performance inertial sensor based on the Sagnac effect, designed for high-precision inertial navigation systems (INS). It measures angular increments by detecting the phase difference between counter-propagating laser beams within a closed monolithic glass cavity, delivering accurate and stable angular rate information.
With high integration, excellent long-term stability, and strong environmental adaptability, the Dubhe-90 RLG has become a preferred solution for space-grade and high-end navigation applications worldwide.
The Dubhe-90 Ring Laser Gyroscope is widely used in:
Spacecraft and launch vehicles
Aircraft and UAV inertial navigation systems
Satellites and space platforms
Land vehicles and autonomous systems
Marine vessels and submarines
High-precision attitude and heading reference systems (AHRS)
Monolithic optical and electronic integration, enabling easy installation and high system reliability
Compact and lightweight design with optimized and controlled power consumption
High reliability with strong resistance to shock and vibration, suitable for harsh environments
Wide dynamic response bandwidth with high-resolution digital output, supporting real-time navigation and control
The Dubhe-90 RLG provides ultra-low bias drift, stable performance, and long operational life, making it an ideal core sensor for advanced INS, navigation, and attitude reference systems.
| 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 | |