Aiming at de-tumbling a non-cooperative space target safely and efficiently, an eddy brake approach utilizing multiple high-temperature superconducting (HTS) coils is proposed in this paper. The configuration design criteria of HTS coil are constructed first to guarantee the validity of the eddy brake method. Then, considering that each HTS coil is mounted on a servicing satellite, the desired position and attitude of each servicing satellite is calculated to meet the design criteria. Next, the eddy brake process is analyzed, where how to generate and keep the desired magnetic field is considered, and then the angular velocity decay process of the target is presented. Concretely, a nonlinear control law utilizing the consensus theory is adopted to achieve and keep the desired formation of the multi-satellite system. Finally, numerical simulations are carried out to testify the proposed method using different number servicing satellites, and the simulation results verify the effectiveness of the proposed method.

针对非合作空间目标安全有效地去翻滚，本文提出了一种利用多个高温超导（HTS）线圈的涡流制动方法。首先构建了高温超导线圈的配置设计准则，以保证涡流制动方法的有效性。然后，考虑到每个 HTS 线圈都安装在服务卫星上，计算每个服务卫星的所需位置和姿态以满足设计标准。接着分析了涡流制动过程，考虑了如何产生和保持所需的磁场，然后给出了目标的角速度衰减过程。具体而言，采用了利用一致性理论的非线性控制律来实现并保持多卫星系统的期望形成。最后，