Full-Text Search:
Home|Journal Papers|About CNKI|User Service|FAQ|Contact Us|中文
Add to Favorite Get Latest Update

A Study on Soft-Ianding Orbit of Lunar Detector

Zeng Guoqiang; Zhao Hanyuan; Xi Xiaoning(Department of Automatic Control, NUDT, Changsha, 410073)  
In this paper, braking scheme and orbital optimization are discussed, assuming that the lunar detector approaches the moon vertically.
【CateGory Index】: V423.6
Download(CAJ format) Download(PDF format)
CAJViewer7.0 supports all the CNKI file formats; AdobeReader only supports the PDF format.
Chinese Journal Full-text Database 5 Hits
1 Ma Wenzhen Zheng Jianhua(Center for Space Science and Applied Research,Chinese Academy of Sciences,Beijing 100080,China)Gao Changsheng(School of Aerospace,Harbin Institute of Technology,Harbin 150001,China);Trajectories to the far side of the sun via gravity assists[J];Journal of Beijing University of Aeronautics and Astronautics;2006-08
2 Sun Baochen,Rong Siyuan(Harbin Institute of Technology,Harbin,150001);Error Analysis of Flight Trajectory to the Moon[J];Missiles and Space Vehicles;2006-06
3 Cui Shaochun (Beijing Institute of Space Mechanics & Electricity, Beijing 100076);Flight to the Moon[J];Spacecraft Recoery & Remote Sensing;2002-01
4 Jia Puzhao(Beijing Institute of Spacecraft Environment Engineering,Beijing 100094,China);The design of a steady state acceleration simulation test equipment-centrifuge(1~(st) part)[J];Spacecraft Environment Engineering;2009-01
5 DING Zhen-quan,GAO Hai-bo,DENG Zong-quan(School of Mechanical and Electricity of Harbin Institute of Technology,Harbin 150001,China);Dynamic analysis of locking-releasing mechanism for side-load lunar rover[J];Machinery Design & Manufacture;2008-03
Chinese Journal Full-text Database 10 Hits
1 Wang Jie Cui Naigang Liu Dun (Harbin Institute of Technology,Harbin,150001)$$$$;Study on Lunar Soft Landing by the Method of Establishment of the Lunar Perpendicular[J];MISSILES AND SPACE VEHICLES;2000-04
2 Lin Shengyong(Northwestern Polytechnical University,Xi'an,710072)Li Zhuji He Xingsuo (Aerospace System Engineering Shanghai,Shanghai,201108);Some Characteristics of Trans-lunar Trajectory[J];Missiles and Space Vehicles;2004-03
3 Zhou Tianshuai,Li Dong,Chen Xinmin,Yang Hujun(Beijing Institude of Astronautical System Engineering ,Beijing, 100076);Application of Foreign Spacecrafts of Sun-Earth Libration Points and Manners of Transfer Trajectory[J];Missiles and Space Vehicles;2004-05
4 OUYANG Zi-yuan (1.Institute of Geochemistry, CAS, Guiyang 550002,China; (2.National Astronomical Observatories, CAS, Beijing 100012,China);SCIENTIFIC OBJECTIVES OF CHINESE LUNAR EXPLORATION PROJECT AND DEVELOPMENT STRATEGY[J];Advance in Earth Sciences;2004-03
5 Ren Xuan (Department of Automatic Control, NUDT, Changsha, 410073)Chen Jianxiang (Beijing Institute of System Engineering, Beijing, 100101);Characteristics and Approximate Solutions of Normalimpact Transfer Trajectory to the Moon[J];JOURNAL OF NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY;1997-06
6 ZENG Guo qiang,REN Xuan,XI Xiao ning (College of Aerospace and Material Engineering, National Univ. of Defence Technology, Changsha 410073 China);An Algebraic Method for Fast Design of Lunar Satellite Transfer Trajectory[J];JOURNAL OF NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY;2000-02
7 Wang Jie , Cui Naigang, Liu Dun , Li Junfeng ( Laboratory of Dynamics & Cbntrol, Department of Engineering Mechanics, Tsinghua University, Beijing 100084) ( Laboratory of Flight Dynamics & Cbntrol, Department of Aerospace Engineering and Mechanics, Harbin Institute of Technology, Harbin 150001);Study on Soft-landing Trajectories of Constant-thrust-amplitude Lunar Probe[J];High Technology Letters;2003-04
8 Zong Hong Li Tieshou Wang Dayi Beijing Institute of Control Engineering, Beijing 100080;Conception on GNC System for Lunar Satellite[J];Aerospace Control;2005-01
9 Wei Yanming Ren Kun Zhang Bing Beijing Institute of Control Engineering, Beijing 100080;Preliminary Conception on Propulsion Systems for Chinese Lunar Exploration Project[J];Aerospace Control;2005-01
10 Shan Yongzheng Duan Guangren Liu Hongliang Center for Control Theory and Guidance Technology,Harbin Institute of Technology,Harbin 150001,China;Soft Landing Optimal Terminal Guidance Strategy of Lunar Probe[J];Aerospace Control;2006-05
©2006 Tsinghua Tongfang Knowledge Network Technology Co., Ltd.(Beijing)(TTKN) All rights reserved