多碎片清除任务设计：基于Lambert制导的远距离导引段燃料消耗估算

The spacecraft rendezvous and docking process generally consists of four stages: far range guidance, close range guidance, translation and approach, and docking [15-16]. This article focuses on the design of multi-debris removal tasks, and the guidance method adopts Lambert guidance to estimate the fuel consumption required for the satellite to release the spacecraft to capture debris and for the spacecraft to continuously remove debris in the far range guidance stage algorithm.