期刊文献+

行星着陆自主导航与制导控制研究现状与趋势 被引量:19

Research Status and Developing Trend of the Autonomous Navigation, Guidance, and Control for Planetary Landing
下载PDF
导出
摘要 行星着陆自主导航与制导控制技术是行星着陆过程的核心技术之一,关系到行星着陆任务的成败。本文基于未来火星和小天体着陆对自主导航与制导控制技术的发展需求,阐述了进一步开展自主导航与制导控制研究的必要性,围绕行星着陆过程环境特点,分析了自主导航与制导控制技术所遇到的挑战,随后概括了行星着陆自主导航与制导控制所涉及的关键技术,并综述了关键技术的研究现状。最后对我国未来行星着陆探测自主导航与制导控制技术的发展方向进行了展望。 Autonomous navigation,guidance,and control is one of the key technologies for planetary landing,which has adirect impact on mission success. In this paper,the necessity and importance of the further research on the autonomousnavigation,guidance,and control are elaborated focusing on the developing demand for the Mars and small body landing missionin the future. Based on the environment features,the challenges encountered for the autonomous navigation,guidance,andcontrol are analyzed. Then and the key techniques involved are discussed,and the state-of-the-art techniques and research tendencyof the autonomous navigation for planetary landing are summarized. Finally,the development trends of the autonomousnavigation,guidance,and control for Chinese planetary landing mission in the future are previewed.
作者 于正湜 崔平远 YU Zhengshi;CUI Pingyuan(Institute of Deep Space Exploration,Beijing Institute of Technology,Beijing 100081,China;Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration,Ministry of Industry and Information Technology,Beijing 100081,China;Key Laboratory of Dynamics and Control of Flight Vehicle,Ministry of Education,Beijing 100081,China)
出处 《深空探测学报》 2016年第4期345-355,共11页 Journal Of Deep Space Exploration
基金 国家重点基础研究发展计划(2012CB720000) 国家自然科学基金资助项目(61374216 61304248 61304226) 北京理工大学创新团队基金资助项目
关键词 行星着陆 火星 小天体 自主导航 制导控制 planetary landing Mars small body autonomous navigation guidance and control
  • 相关文献

参考文献11

二级参考文献309

  • 1孙军伟,崔平远.月球软着陆多项式制导控制方法[J].宇航学报,2007,28(5):1171-1174. 被引量:6
  • 2CUI PingYuan1,QIAO Dong1,CUI HuTao2 & LUAN EnJie3 1 School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China,2 Harbin Institute of Technology,Harbin 150001,China,3 National Defense Science and Industry Bureau,Beijing 100048,China.Target selection and transfer trajectories design for exploring asteroid mission[J].Science China(Technological Sciences),2010,53(4):1150-1158. 被引量:15
  • 3Johnson A E, Matthies L H. Precise image based motion estimalion for autonomous small body exploration [ C ]//Proceedings of the Fifth International Symposium on Artificial Intelligence, Robotics and Automation in Space, Noordwijk, Netherlands, European Space Agency, 1999: 627 - 634. 被引量:1
  • 4Misu T, Hashimoto T, Ninomiya K. Optical guidance for autonomous landing of spacecraft [J]. IEEE Transactions on Aerospace and Electronic Systems, 1999, 35(2) :459 - 472. 被引量:1
  • 5Benedetti A, Perona P. Real-time 2 - D feature detection on a reconfigurable computer [ C ]//Proceedings of the IEEE Computer Society Conference on Computer Vision and Pattern Recognition, Washington, DC, USA, IEEE Computer Society, 1998: 586-593. 被引量:1
  • 6Shi J, Tomasi C. Good feature to track[ C]//IEEE International Conference on Computer Vision and Pattern Recognition, Berlin, IEEE Computer Society Press, 1993 : 593 - 600. 被引量:1
  • 7Broida J, Chandrashekhar S, Chellappa R. Recursive 3-D motion estimation from a monocular image sequence [ J ]. IEEE Transactions on Aerospace and Electronic Systems, 1990, 26(4) :639 - 656. 被引量:1
  • 8Seidensticker K J, Mohlmann D, Apathy I, et al. SESAME-an experiment of the Rosetta Lander Philae: objectives and general design [ J ]. Space Science Reviews 2007, 128(1): 301- 337. 被引量:1
  • 9Li S, Cui P Y, Cui H T. Autonomous navigation and guidance for landing on asteroids[J]. Aerospace Science and Technology, 2006, 10(3): 239-247. 被引量:1
  • 10Hashimoto T, Kubota T, Sawai S. Image-based guidance, navigation, and control for MUSES -C sample and return spacecraft[J]. Advances in the Astronautical Sciences, 2002, 111: 181 -192. 被引量:1

共引文献278

同被引文献232

引证文献19

二级引证文献78

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