系统工程与电子技术 ›› 2026, Vol. 48 ›› Issue (11): 4008-4016.doi: 10.12305/j.issn.1001-506X.2026.11.30

• 制导、导航与控制 • 上一篇    下一篇

考虑轨道机动的多星协同对地观测链生成方法

陈渊1,2(), 秦垚1, 敬丹1, 张进2   

  1. 1. 中国工程物理研究院总体工程研究所,四川 绵阳 621999
    2. 国防科技大学空天科学学院,湖南 长沙 410073
  • 收稿日期:2025-07-11 修回日期:2025-11-08 出版日期:2026-10-25 发布日期:2026-02-12
  • 通讯作者: 张进 E-mail:sairen@whu.edu.cn
  • 作者简介:陈 渊(1999—),男,助理工程师,硕士,主要研究方向为航天任务仿真、优化算法
    秦 垚(1995—),男,工程师,硕士,主要研究方向为系统工程
    敬 丹(1984—),女,高级工程师,硕士,主要研究方向为系统工程

Multi-satellite cooperative Earth observation link generation method considering orbital maneuvering

Yuan Chen1,2(), Yao Qin1, Dan Jing1, Jin ZHANG2   

  1. 1. Institute of Systems Engineering,China Academy of Engineering Physics,Mianyang 621999,China
    2. College of Aerospace Science,National University of Defense Technology,Changsha 410073,China
  • Received:2025-07-11 Revised:2025-11-08 Online:2026-10-25 Published:2026-02-12
  • Contact: Jin ZHANG E-mail:sairen@whu.edu.cn

摘要:

某些对地应急观测任务中,需要多颗、多类型的卫星即时、持续地观测,形成一条观测窗口链,以更好地支持 “观测-判断-决策-行动”闭环回路。通过卫星轨道机动的方式调整观测窗口,可在短时间内增加满足时序约束的观测窗口链数量。以轨道机动时刻、大小为优化变量,以轨道机动总成本和观测窗口链总数为目标函数,采用多目标遗传算法求解。结果表明,以平均每颗卫星3 m/s的速度增量,可在12 h内使80颗卫星组合的观测窗口链数量从5条提升到29条,且随着任务时间、窗口间隔时间、速度增量和卫星规模的增大,提升效果将进一步增加,通过轨道机动生成对地观测链的方法有效。

关键词: 对地观测, 轨道机动, 观测窗口链, 多星协同, 任务规划

Abstract:

In some emergency Earth observation missions, multiple and various types of satellites are required to conduct real-time and continuous observations, forming an observation window chain to better support the “observation-orientation-decision-action” closed loop. By adjusting the observation window through satellite orbital maneuvering, the number of observation window chains that meet the temporal constraints can be increased in a short period of time. Taking the orbital maneuvering time and size as the optimization variables, and the total cost of orbital maneuvering and the total number of observation window chains as the objective functions, the multi-objective genetic algorithm is adopted for solution. The results show that with an average speed increment of 3 m/s per satellite, the number of observation window chains of 80 satellite combinations can be increased from 5 to 29 within 12 h. Moreover, with the increase of mission time, window interval time, speed increment and satellite scale, the improvement effect will be further enhanced. The method of generating Earth observation chains through orbital maneuvers is effective.

Key words: Earth observation, orbital maneuvering, observation window chain, multi-satellite collaboration, mission planning

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