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.

ParameterValue

Capacity of air-floating platform1000-2000 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 measurement1 ()
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°