Satellite encounters during close operations, such as rendezvous, formation, and cluster
flights, are typical long-term encounters. The collision probability in such an encounter is a …

The conventional reachable domain problem for satellites with a single impulse under the
ideal two-body dynamical environment was extended to a more realistic scenario that takes …

Orbital pursuit–evasion (OPE) has garnered significant attention due to its potential
applications in space rendezvous and proximity operations. Conventional methods using …

ORBITAL maneuvers, particularly impulse maneuvers with a high thrust, are crucial in the
design of space missions involving spacecraft rendezvous [1, 2], collision avoidance [3], and …

This work establishes a general-purpose method for computing the exact boundary of the
reachable set in a specified direction, with additional constraints imposed on the terminal …

Purpose Lots of successful space missions require that the maneuvering spacecraft can
reach the target spacecraft. Therefore, research on relative reachable domain (RRD) in …

为提高空间非合作目标近距离逼近轨迹的安全性, 同时对接近时间及所消耗燃料进行优化,
针对空间失效自旋非合作目标近距离接近问题, 给出了失效卫星动态安全走廊 …

航天器轨道机动可达域是空间态势的有效表征方法, 对空间目标机动监测,
威胁评估和碰撞预警等有重要意义. 特别地, 地固系下的轨道机动可达域对分析机动卫星星下点 …

In order to improve the safety of non-cooperative target's close-range approach trajectory,
and optimize the approach time and fuel consumption at the same time, this paper designs …

Multi-spacecraft missions have gained significant attention in recent years due to their
improved affordability, scalability, adaptability, and redundancies over traditional monolithic …