李爽

个人信息Personal Information

教授

招生学科专业:
控制科学与工程 -- 【招收博士、硕士研究生】 -- 航天学院
航空宇航科学与技术 -- 【招收博士、硕士研究生】 -- 航天学院
电子信息 -- 【招收博士、硕士研究生】 -- 航天学院
机械 -- 【招收博士、硕士研究生】 -- 航天学院

毕业院校:哈尔滨工业大学

学历:哈尔滨工业大学

学位:工学博士学位

所在单位:航天学院

办公地点:江宁校区D11号楼A503

联系方式:025-84896039

电子邮箱:

扫描关注

论文成果

当前位置: 中文主页 >> 科学研究 >> 论文成果

On-orbit assembly mission planning considering topological constraint and attitude disturbance

点击次数:

所属单位:航天学院

发表刊物:ACTA ASTRONAUTICA

关键字:On-orbit assembly Vibration suppression Mission planning Topological constraint Branch-and-bound method

摘要:This paper investigates the on-orbit assembly mission planning problem of a large space antenna structure. The study is significantly important for the construction of large-scale spatial structures. The flexible connection between the antenna pieces and the topological constraint are taken into consideration. Several innovative approaches are presented to realize the mission planning process. First, the mesh model from the fly net dynamics is adopted and modified to create a mapping between the vibrations of the antenna plate during the assembly process and the assembly path. Second, the geometrical model is developed to implement the topological constraint into the system. Finally, a hybrid method combining the branch-and-bound method and the modified ant colony algorithm is proposed to solve the optimization problem. The simulation results show that the proposed algorithm can efficiently obtain a solution which respects the topological constraint and suppresses the vibration disturbance as much as possible.

ISSN号:0094-5765

是否译文:

发表时间:2018-11-01

合写作者:She, Yuchen,杜炳南,Cao, Kai

通讯作者:李爽