期刊文献+

月球软着陆自主组合导航研究 被引量:3

Autonomous Integrated Navigation for Lunar Soft Landing
原文传递
导出
摘要 针对惯性测量单元(IMU)存在误差积累的特点,提出了利用探测器上的光学敏感器,通过对预先选定的特征点的测量得出探测器的相对位置,根据这些光学导航信息再结合惯性导航输出轨迹,通过多模自适应滤波完成对IMU导航的修正。对整个导航系统的可观性进行了分析,并通过数值仿真验证了所提出的自主导航方法的可行性。 We propose an autonomous navigation scheme based on optical navigation and inertial measurement unit(IMU) for lunar soft landing. In order to remove the accumulation errors of IMU, we use the on-board optical measurement information of pre-selected feature point to obtain relative position of the probe. Then, based on those optical information and the output trajectory of IMU navigation, the amendments of IMU navigation are completed by the multi-model adaptive filtering. In addition, the observability of entire navigation system is analyzed. Finally, the feasibility of the proposed autonomous navigation scheme is confirmed by numerical simulation.
作者 宋敏 袁运斌
出处 《武汉大学学报(信息科学版)》 EI CSCD 北大核心 2010年第9期1013-1016,共4页 Geomatics and Information Science of Wuhan University
基金 国家杰出青年科学基金资助项目(40625013) 国家自然科学基金资助项目(40890160) 国家863计划资助项目(2007AA12Z311)
关键词 月球软着陆 自主组合导航 多模自适应估计 可观性分析 lunar soft landing autonomous integrated navigation multi-model adaptive estimation observability analysis
  • 相关文献

参考文献8

二级参考文献11

  • 1[1]Guizzo G P,Vukman I.Autonomous smart lander simulator based on stereo vision for the descent phase on mars[C]//54th International Astronautical Congress of the International Astronautical Federation,Bremen,Germany:IAF,2003,IAC-03-IAA.10.3.06
  • 2[2]Paar G,Polzleitner W.Autonomous spacecraft navigation using computer vision:A case study for the moon[C]//Proceedings of SPIK -The International Society for Optical Engineering,WA,USA:Society of Photo-Optical Instrumentation Engineer,1995:157-169.
  • 3[3]Pien H.Achieving safe autonomous landings on mars using visionbased approaches[C]// SPIE on Cooperative Intelligent Robotics in Space Ⅱ,1991,1612:24-35
  • 4[5]Bennett F V.Apollo Experience Report-Mission Planning for Lunar Module Descent and Ascent[R].1972:NASA TN D-6846
  • 5[6]Beilock M.Surveyor Lander Mission Capability[R].JPL Technical Report No.32-618,1964,N64-28969
  • 6[7]Beresnev N P,Legonstayev V P.Control System for Automatic Station Lunar-9[R].A67-39167
  • 7[8]Ockels W J.EuroMoon 2000-a plan for a european lunar south pole expedition[J].Acta Astronautica,1996,41(4):579-583
  • 8[9]Mitsuhashi N,Mizuno T.Fundamental development of landing radar for lunar and planetary mission[C]//Proceedings of the 47th Space Sciences and Technology Conference,2003:196-198
  • 9关肇直,陈翰馥执笔,中国科学院数学研究所控制理论研究室.线性控制系统的能控性和能观测性[M]科学出版社,1975.
  • 10任光,朱利民,贾欣乐.多参考模型智能控制器的硬件设计[J].大连海事大学学报,1998,24(2):81-83. 被引量:1

共引文献39

同被引文献20

引证文献3

二级引证文献17

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部