With integrated satellite management, compact designed for Cube-sat, Plug and Play ADCS-N1 is integrated by 2 star trackers, 1 sun sensor, 1 magnetometer, 1 GNSS, 2 Three-axis Gyroscope, 3 megnetic torquer, and 4 reaction wheel.
Pointing Accuracy：better than0.02°
Communication：CAN/RS422
Size：(96±1)mm×(96±1)mm×(100±1)mm
Mass：1.43±0.1kg
| Component | Quantity | Performance |
| Star Tracker | 2 | Accuracy(Pointing/ Roll): 5″ (3σ)/ 50″ (3σ)； |
| Update Rate:10Hz | ||
| Dynamic Performance:2°/s | ||
| Exclusive Angle: Sun:<35°，Earth:<30° | ||
| Sun Sensor | 1 | Accuracy:0.1°(3σ) |
| Update Rate:10Hz | ||
| Field of View: 85° ×85° | ||
| Gyroscope | 2 | Bias Instability: 0.5°/h |
| Angle Random Walk: 0.03° /√ℎ | ||
| Angle Measurement Range: ±300°/s | ||
| Magnetometer | 1 | Magnetic Measuring Range: ±8Gauss |
| Linearity Error: ±1.0%FS | ||
| Measurement Noise:10nT | ||
| Reaction wheel | 4 | Maximum Output Angular Momentum:20mNms |
| Maximum Output Torque:2.5mNm | ||
| Torque Control Accuracy: Better than 0.01mNm | ||
| Rotational Speed Control Accuracy: Better than 1rpm | ||
| Magnetic Torquer | 3 | Maximum Output Magnetic Moment: 0.66A·m²@12V; 0.27A·m²@5V |
| Residual Magnetic Moment: ≤10 mAm2 | ||
| Linearity: Better than 10% | ||
| GNSS | 1 | Position Accuracy: ≤10m |
| Velocity Accuracy: ≤0.1m/s |
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TY-Space Technology (Beijing) Ltd. is professional focusing on advanced attitude optical sensors, especially Star Trackers for space industry.