| Technical Specifications | |
|---|---|
| Place of Origin | China |
| Brand Name | Star & Inertia Technology |
| Model Number | Dubhe-A6 |
| Alignment Time | ≤15min |
| Position Accuracy (Pure Inertia) | ≤1nm/6h, CEP |
| Position Accuracy (INS/GNSS) | Better Than GNSS |
| Speed Accuracy (Pure Inertia) | ≤1.0m/s, RMS |
| Speed Accuracy (INS/GNSS) | ≤0.2m/s, RMS |
| Heading Accuracy (Pure Inertia) | ≤0.02°sec(L), RMS |
| Heading Accuracy (INS/GNSS) | ≤0.01°sec(L), RMS |
| Pitch & Roll Accuracy (Pure Inertia) | ≤0.015°, RMS |
| Pitch & Roll Accuracy (INS/GNSS) | ≤0.01°, RMS |
| Dimensions | 193×169×160mm |
| Weight | ＜6.5kg |
| Temperature Range | -40℃~60℃ |
| Input Voltage | DC24V(±25%) |
| Key Features |
|
Dubhe-A6 Optical Gyros Quartz RLG Aircraft Inertial Navigation System INS For Astroinertial
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