| Equipment | Quantity | Performance |
| Star Tracker | 2 | Accuracy(Pointing:/ Rolling) :3″(3σ) , 30″ (3σ) |
| Update Rate:10Hz | ||
| Dynamic Range:3°/s | ||
| Mass:130g | ||
| Sun Sensor | 2 | Measurement Accuracy:0.1°(3σ) |
| Update Rate:5Hz | ||
| Mass:10g | ||
| Gyroscope | 1 | Bias Stability:0.5°/h |
| Angle Random Walk:0.15°/√h | ||
| Velocity Ratio Measuring Range: ±40°/s | ||
| Magnetometer | 1 | Magnetic Measuring Range: ±8Gauss |
| Linearity Error: ±0.1%FS | ||
| Magnetic Field ldentification:2 milli-Gauss | ||
| Reaction Flywheel | 4 | Max Output Angular Momentum:15mNms |
| Max Output Force Moment:2.5mNm | ||
| Speed Control Accuracy:≥±3rpm | ||
| Force Moment Control Accuracy:≥0.02mNm | ||
| Magnetic Torquer | 3 | Max Output Magnetic Dipoe Moment:10Am² |
| Residual Magnetic Moment:＜1% | ||
| Linearity:≥5% | ||
| Attitude Controller | 1 | High Attitude Accuracy:0.02° |
| Basic Attitude Accuracy:≥3° |
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TY-Space Technology (Beijing) Ltd. is professional focusing on advanced attitude optical sensors, especially Star Trackers for space industry.
