摘要
在自主空间交会任务中,星载量测系统的测量精度会对末端控制效果产生较大的影响。文章从自主近程导引的多脉冲控制律出发,通过解析方法分析测量误差对多脉冲控制精度的影响,并在此基础上,提出一种逆向算法以解决当指定导引的末端控制精度要求时,如何确定相应的测量误差的允许范围才能满足所期望的控制效果。最后仿真表明,通过逆向算法获得的测量允许误差,可以理想地达到要求的末端控制精度。
Aim.The introduction of the full paper reviews Refs.1 through 11 and points out that there is an urgent need to explore but,to our knowledge,no paper in the open literature that explores the effect of measurement error on control precision.Sections 1 and 2 explain the results of our exploration.Their core consists of： a detailed study of the relationship between measurement error and control precision was performed via the reverse arithmetic in the area of autonomous rendezvous.The reverse arithmetic is based on the well-known theory of C-W rendezvous multi-impulse;the research on the effect of measurement error on control precision was carried out analytically based on the multi-impulse theory.And the reverse arithmetic was put forward to solve the problem of how much measurement error is allowable.The simulation results,given in Figs.4,5 and 6,and their analysis show preliminarily that the maximum permissible measurement error estimated by the reverse arithmetic is effective for the required control error.
出处
《西北工业大学学报》
EI
CAS
CSCD
北大核心
2010年第4期481-485,共5页
Journal of Northwestern Polytechnical University
基金
航天科技创新基金(CSAC200902)
空间智能控制技术国防科技重点实验室基金(SIC07020301)资助
关键词
自主交会
相对导航
测量精度
控制精度
多脉冲控制
orbits
measurement errors
control
autonomous rendezvous
control precision
multi-impulse control
作者简介
吕纪远（1984-），西北工业大学博士研究生，主要从事航天器导航与控制方面的研究。
