High Precision TDLG90S Ring Laser Gyroscope
The TDLG90S Ring Laser Gyroscope operates on the Sagnac effect principle, utilizing interference phase differences between clockwise and counterclockwise laser beams within a closed resonant cavity to precisely measure angular increments. This gyroscope features high integration, exceptional reliability, strong environmental adaptability, and stable operational performance, making it a core sensor in high-precision inertial navigation systems.
Applications
Certified for integration with inertial navigation systems (INS) and attitude heading reference systems (AHRS) across:
- Aerospace platforms (spacecraft/aircraft/satellites)
- Marine systems (surface vessels/submersibles)
- Terrestrial navigation modules (automotive vehicles)
Key Characteristics
- Integrated light path and circuit design with simple structure for easy installation
- Compact size, lightweight construction, and controllable power consumption
- High reliability with excellent shock and vibration resistance
- Strong environmental adaptability and stable operational performance
- Wide dynamic response bandwidth with digital signal output
Technical Specifications
| Performance Parameter |
Specification |
| Bias stability (1σ) |
0.004°/h ~ 0.002°/h |
| Zero bias repeatability (1σ) |
0.002°/h ~ 0.001°/h |
| Angular Random Walk (ARW) |
0.0007°/√hr ~ 0.0004°/√hr |
| Scale factor error (1σ) |
≤ 2ppm |
| Dynamic Range |
≥ ±400°/s |
| Bandwidth |
> 200Hz |
| 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℃ |
| Power supply |
±15V, ±5V |
| Connector (25 pins) |
J30JM-37ZKP36 |
| Power consumption |
≤ 3W |
| MTBF (per MIL-HDBK-217-F) |
> 10,000 hours |
| Weight |
2kg |
| Dimensions |
151mm * 126mm * 57mm |