Research Article
Compound Attitude Maneuver and Collision Avoiding Control for a Novel Noncontact Close-Proximity Formation Satellite Architecture
Table 1
Related parameters of physical system platform.
| Parameter | Value |
| Capacity of air-floating platform | 1000-2000 kg | Rotation range of air-floating platform | ±25° (-axis) | Centroid fine adjustment error of air-floating platform | ≤0.2 kgm | Centroid coarse adjustment error of air-floating platform | ≤5 gcm | System total interference torque of air-floating platform | ≤0.1 Nm | Dynamic range of wide-range angle measurement | ±30° | Accuracy of wide-range angle measurement | 1 () | Angular momentum of control moment gyroscope | ≤210 Nms | Output torque of control moment gyroscope | ≤55 Nm | Frame angular velocity stability of control moment gyroscope | | Output force of noncontact Lorentz actuator | ≤15 N | Air-gap constraint of noncontact Lorentz actuator | ±0.9° |
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