I. Introduction
On-orbit service (OOS) is essential for the space environment since it can rescue failed spacecraft or remove orbital debris, especially in the case of the widespread utility of mega-constellation [1], [2], [3]. A key aspect of OOS is to achieve ultraclose-range proximity maneuvers. The servicing spacecraft (chaser) can approach the target through proximity maneuvers under collision avoidance constraints. However, in the ultraclose range, the relative distance between the two spacecraft is comparable to their scale. Neglecting either spacecraft's slender structures (solar panels or antenna) will result in a collision. In addition, the relative attitude of the two spacecraft interacts with their complex shape, making the construction of collision avoidance constraints more difficult. There is an urgent need to address the safety problems caused by the two spacecraft's complex shapes and relative attitude during the ultra-close-range proximity.