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崔平远

  • 职称:教授
  • 研究方向:深空探测器自主导航与制导、轨道设计与优化
  • 所属院系:宇航学院   副院长
  • 成果数量:299条,属于本单位的个人成果299条
  • 学术称号:973首席科学家
  • 简介: 【人物简介】崔平远,北京理工大学首批特聘教授,校学术委员会委员,机械与运载学部副主任委员,深空探测技术研究所所长,小天体探测与防御实验室主任,“深空自主导航与控制”工信部重点实验室主任,国家973计划项目首席科学家,享受国务院政府特殊津贴。兼任国务院学位委员会航空宇航科学与技术学科评议组成员,探月与航天工程中心“月球与深空探测国际合作工作...

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作者: Yu, Zhengshi1( yuzhengshi@gmail.com);Cui, Pingyuan1( cuipy@bit.edu.cn);Zhu, Shengying1( zhushengying@gmail.com) (1School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, People’s Republic of China)

出处: Advances in Space Research 2014 Vol.54No.8 P1513-1524

关键词: Observability;Mars entry navigation;Fisher information matrix;Radiometric measurements;Geometric configuration

摘要: A thorough observability analysis of the Mars entry navigation using radiometric measurements from ground based beacons is performed. This analysis in ...

被引情况: sci被引 7 次

作者: Haibin Shang E-mail the corresponding author E-mail the corresponding author Author Vitae;Shuai WangCorresponding author contact information Corresponding author contact information , E-mail the corresponding author E-mail the corresponding author Author Vitae;Pingyuan Cui E-mail the corresponding author E-mail the corresponding author Author Vitae (Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing Institute of Technology, Beijing 100081, China)

出处: Chinese Journal of Aeronautics 2014 Vol.27No.2 P338-348

作者: Ya-Min Wang;Dong Qiao;Ping-Yuan Cui (1. School of Aerospace Engineering, Beijing Institute of Technology, 100081, Beijing, China2. Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, 100081, Beijing, China)

出处: Acta Mechanica Sinica 2014 Vol.30No.6 P966-972

关键词: Lunar orbit;Asteroid exploration;Low-energy transfer;Sun-Earth-Moon system

摘要: Asteroid exploration trajectories which start from a lunar orbit are investigated in this work. It is assumed that the probe departs from lunar orbit ...

被引情况: sci被引 1 次

作者: Dong Qiaoa, , ;Pingyuan Cuia;Yamin Wanga;Jiangchuan Huangb;Linzhi Mengb;Degang Jiec (a School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, Chinab China Academy of Space Technology, Beijing 100093, Chinac Lunar Exploration and Aerospace Engineering Center, Beijing 100037, China)

出处: Advances in Space Research 2014 Vol.54No.10 P2087-2093

关键词: Chang’E-2;Lissajous orbit;Four-body problem;Transfer trajectory;Analysis of tracking and control

摘要: Chang’E-2 (CE-2) has firstly successfully achieved the exploring mission from lunar orbit to Sun–Earth L2 region. In this paper, we discuss the design ...

被引情况: sci被引 4 次

作者: Tong Qin;Shengying Zhu, ;Pingyuan Cui;Ai Gao (Institute of Deep Space Exploration, School of Aerospace Engineering, Beijing Institute of Technology, Mail box 22, Beijing 100081, People’s Republic of ChinaKey Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100081, People’s Republic of China)

出处: Advances in Space Research 2014 Vol.54No.9 P1888-1900

关键词: Pinpoint landing;Powered descent phase;Integrated Doppler radar;Mars Orbiter

摘要: Pinpoint landing (within 100 m from the target) is essential for future Mars exploration missions. This paper deals with one aspect of the pinpoint la ...

被引情况: sci被引 4 次

作者: Cui, Pingyuan(1,2); Xu, Rui(1,2); Zhu, Shengying(1,2); Zhao, Fanyu(1,2) ((1) Institute of Deep Space Exploration, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China; (2) Key Lab of Flight Vehicle Dynamics and Control of MOE, Beijing 100081, China)

出处: Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica 2014 Vol.35No.1 P13-28

关键词: Planning - Recovery - Telemetering

摘要: During the process of deep space exploration, the explorer is far away from the Earth while the environment around it is complex and harsh. Therefore ...

作者: Shang, Hai-Bin(1,2); Cui, Ping-Yuan(1,2); Wang, Shuai(1,2); Dou, Qiang(1,2) ((1) Institute of Deep Space Exploration, Beijing Institute of Technology, Beijing, China; (2) Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing, China)

出处: Yuhang Xuebao/Journal of Astronautics 2014 Vol.35No.11 P1245-1253

关键词: Algorithms - Computational efficiency - Genetic algorithms - Image matching - Interplanetary spacecraft - Orbital transfer - Orbits - Polynomial approximation

摘要: In this paper, the multi-objective optimization of Halo-to-Halo transfer trajectory between different Sun-planet systems is discussed by considering t ...

作者: Chen, De-Xiang(1,2); Xu, Rui(1,2); Cui, Ping-Yuan(1,2) ((1) Institute of Deep Space Exploration Technology, Beijing Institute of Technology, Beijing 100081, China; (2) Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100081, China)

出处: Yuhang Xuebao/Journal of Astronautics 2014 Vol.35No.6 P669-676

关键词: Computer simulation - Processing

摘要: Considering the limited resource, complex constraint and parallel activities, autonomous planning of spacecraft mission is investigated in this paper. ...

作者: Cui, Ping-Yuan(1,2); Dou, Qiang(1,2); Gao, Ai(1,2) ((1) School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China; (2) Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100081, China)

出处: Yuhang Xuebao/Journal of Astronautics 2014 Vol.35No.1 P1-12

关键词: Interplanetary flight - Martian surface analysis - Plasma sheaths

摘要: Based on the future Chinese Mars mission, firstly a brief review of previous successful Mars landing is given. Followed by above, the cause of blackou ...

作者: Chen, Jian-Qing(1); Zhu, Sheng-Ying(2,3); Cui, Hu-Tao(1); Cui, Ping-Yuan(1,2,3) ((1) Deep Space Exploration Research Center, Harbin Institute of Technology, Harbin, China; (2) School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China; (3) Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing, China)

出处: Yuhang Xuebao/Journal of Astronautics 2014 Vol.35No.8 P908-915

关键词: Automobile bodies - Image segmentation - Landforms - Landing - Navigation

摘要: An autonomous crater detection method based on the image gray value feature is proposed in this paper. In this method, region of interest (ROI) is use ...

崔平远教授简介



【人物简介】

崔平远,北京理工大学首批特聘教授,校学术委员会委员,机械与运载学部副主任委员,深空探测技术研究所所长,小天体探测与防御实验室主任,“深空自主导航与控制”工信部重点实验室主任,国家973计划项目首席科学家,享受国务院政府特殊津贴。


兼任国务院学位委员会航空宇航科学与技术学科评议组成员,探月与航天工程中心“月球与深空探测国际合作工作组”成员,“宇航智能控制技术”国家级重点实验室学术委员会委员,中国宇航学会理事、深空探测技术专业委员会副主任委员,《深空探测学报》常务副主编、《自动化学报》和《宇航学报》编委。

从事深空探测器自主导航与控制、轨道设计与优化等研究工作。主持973计划项目—“行星表面精确着陆导航与制导控制问题研究”,提出了火星着陆自主导航方案和方法、弱引力小天体自主附着主动控制思想和方法、地外天体着陆区评估“安全因子”概念和评价方法、深空探测轨道优化和小天体目标选择方法。

研制了火星着陆自主导航与制导控制综合仿真系统、小行星自主附着技术集成验证系统、深空环境虚拟仿真与三维可视化演示系统、深空探测目标选择和任务轨道设计平台,成功应用于“嫦娥二号”飞越探测图塔蒂斯小行星的目标选择和轨道设计。


    获国家科技进步二等奖1项,省部级科技奖10项,获授权国家发明专利40项;近五年在宇航领域顶级学术期刊发表论文5篇、重要学术期刊发表论文5篇,出版专著2本。