高级检索
彭德云, 谢剑锋, 赵凤才, 梁爽, 陈翔, 张爱成. 月球采样返回飞控任务多目标协同规划设计[J]. 深空探测学报(中英文), 2022, 9(2): 191-201. DOI: 10.15982/j.issn.2096-9287.2022.20210082
引用本文: 彭德云, 谢剑锋, 赵凤才, 梁爽, 陈翔, 张爱成. 月球采样返回飞控任务多目标协同规划设计[J]. 深空探测学报(中英文), 2022, 9(2): 191-201. DOI: 10.15982/j.issn.2096-9287.2022.20210082
PENG Deyun, XIE Jianfeng, ZHAO Fengcai, LIANG Shuang, CHEN Xiang, ZHANG Aicheng. Collaborative Planning Design of Multi-Targets for Lunar Sampling Return Flight Control Task[J]. Journal of Deep Space Exploration, 2022, 9(2): 191-201. DOI: 10.15982/j.issn.2096-9287.2022.20210082
Citation: PENG Deyun, XIE Jianfeng, ZHAO Fengcai, LIANG Shuang, CHEN Xiang, ZHANG Aicheng. Collaborative Planning Design of Multi-Targets for Lunar Sampling Return Flight Control Task[J]. Journal of Deep Space Exploration, 2022, 9(2): 191-201. DOI: 10.15982/j.issn.2096-9287.2022.20210082

月球采样返回飞控任务多目标协同规划设计

Collaborative Planning Design of Multi-Targets for Lunar Sampling Return Flight Control Task

  • 摘要: 基于月球采样返回任务飞行过程复杂、四器多组合模态协同控制复杂、多类约束关联组合复杂、多种关键控制密集难点,提出了月面采样返回飞行控制任务多目标协同规划设计,确保多目标在轨密集指令与各类型测控资源安排协同有序。分析了月球采样返回与以往月面软着陆和近地交会对接任务的继承差异,设计了复杂多目标器间代传上行控制关系描述、多目标测控资源分配和多目标事件规划方法。“嫦娥五号”在轨任务飞行控制应用表明所作设计是合理可行的。

     

    Abstract: To deal with the difficulties of complex return flight process, complex coordinated control of four-explorers multi-combination modalities, related combination of multiple constraints and a variety of key intensive controls, a multi-objective collaborative planning for lunar sampling return was proposed in order to ensure that the intensive command arrangement of the multiple objectives and the various types of TT&C resources were coordinated and ordered. In this paper, the inheritance difference between the lunar sampling return and the previous lunar soft landing and near-Earth rendezvous and docking missions was analyzed. A description method of the uplink control relationship between complex multi-objective devices, a multi-objectives measurement and control resource allocation method and a multi-objectives event planning method were designed. The flight control application of Chang’E 5 on-orbit mission shows that the design is reasonable and feasible.

     

/

返回文章
返回