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Analysis of GNC Technology in the Whole Process of Landing System of Mars Science Laboratory
- WANG Ziwei, GUO Yanning, LIU Bing
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Department of Control Science and Engineering,Harbin Institute of Technology,Harbin 150001,China
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Received |
Revised |
Published |
05 Oct 2015 |
09 May 2016 |
06 Jun 2022 |
Issue Date |
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20 May 2022 |
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References
[1] Major J. NASA Mars Rover’s risky landing plan:a step-by-step guide. [EB/OL]. (2012-08-03). http://www.space.com/16878-mars-rover-landing-sky-crane-guide.html.
[2] Way D W,Powell R W,Chen A,et al. Mars Science Laboratory:entry,descent,and landing system performance [C]//IEEE Aerospace Conference.[S. l.]:IEEE,2006:1467-1501.
[3] 崔平远,高艾,于正湜. 火星着陆自主导航方案研究进展[J]. 深空探测学报,2014,1(4):18-27
Cui P Y,Gao A,Yu Z S.Research progress of autonomous navigation scheme for Mars landing[J]. Journal of Deep Space Exploration,2014,1(4):18-27
[4] 陈荣芳,夏元清. 火星表面精确着陆制导控制问题研究[D]. 北京:北京理工大学,2014.
Chen R F,Xia Y Q. Research on guidance and control method for Mars precision landing[D]. Beijing:Beijing Institute of Technology,2014.
[5] 崔平远,胡海静,朱圣英. 火星精确着陆制导问题分析与展望[J]. 宇航学报,2014,35(3):246-252
Cui P Y,Hu J H,Zhu S Y.Analysis and prospect of guidance aspects for Mars precision landing[J]. Journal of Astronautics,2014,35(3):246-252
[6] Quadrelli M B,Wood L J,Riedel J E,et al. Guidance,navigation,and control technology assessment for future planetary science missions [J] Journal of Guidance,Control and Dynamics. 2015,38(7):1165-1186
[7] Brugarolas P B,Sam Martin A M,Wong E C. Entry attitude controller for the Mars Science Laboratory [C]//Aerospace. Conf. Big Sky MT:[s. n.],2007.
[8] Acikmese B,Sell S W,San Martin A M. Mars Science Laboratory flyaway guidance,navigation,and control system design[J]. Journal of Spacecraft and Rockets,2014,51(4)1227-1236
[9] 冯军华. 月球软着陆障碍检测与规避控制方法研究[D]哈尔滨:哈尔滨工业大学,2007.
Feng J H. Research on obstacle detection and avoidance control for Moon soft landing[D]. Harbin:Harbin Institute of Technology,2007.
[10] Lafieur J M,Cerimele C J. Mars entry bank profile design for terminal state optimization [C]//AIAA Atmosphere Flight Mechanics Conference and Exhibit. Honolulu,Hawaii:[s. n.],2008.
[11] Garcia-Llama E,Winski R G,Shidner J D,et al. Mars Science Laboratory entry guidance improvements study for the Mars 2018 Mission [C]//Aerospace Conference,2012 IEEE. Big Sky:IEEE,2012.
[12] Adams D S,Ribellim T P. Mars Science Laboratory’s parachute qualification approach [C]//AIAA Aerodynamic Decelarator System Technologythe Conference and Seminar <BR>. Seattle,Washington:AIAA,2009.
[13] Steinfeldt B A,Grant M J,Mate D A,et al. Guidance,navigation,and control system performance trades for Mars pinpoint landing [J]. Journal of Spacecraft and Rockets,2010,47(1):188-198
[14] 修运乐. 火星大气进入轨迹优化与制导方法研究[D]. 南京:南京航空航天大学,2014.
Xiu Y L. Study on Mars atmospheric entry trajectory optimization and guidance[D]. Nanjing:Nanjing University of Aeronautics and Astronautics,2014.
[15] 袁克非,袁赣南. 组合导航系统多源信息融合关键技术研究[D]. 哈尔滨:哈尔滨工程大学,2012.
Yuan K F,Yuan G N. Key technique of multi-source information fusion in integrated navigation system[D]. Harbin:Harbin Engineering University,2012.
[16] Morabito D D. The spacecraft communications blackout problem encountered during passage or entry of planetary atmospheres[R]. Pasadena,California.:Jet Propulsion Laboratory,2002.
[17] 洪晓瑜. VLBI技术的发展和“嫦娥工程”中的应用[J]. 自然杂志,2007,29(5):297-299
Hong X Y. VLBI techniques and application in the Chang′e Lunar Orbiter [J]. Chinese Journal of Nature,29(5):297-299
[18] 卫剑征,谭惠丰,王伟志,等. 充气式再入减速器研究最新进展[J]. 宇航学报,2013,34(7):882-890
Wei J Z,Tan H F,Wang W Z,New trends in inflatable re-entry aeroshell [J]. Journal of Astronautics,2013,34(7):882-890
[19] 李爽,彭玉明,陆宇平. 火星EDL导航、制导与控制技术综述与展望[J]. 宇航学报,2010,31(3):622-626
Li S,Peng Y M,Lu Y P. Review and prospect of Mars EDL navigation guidance and control technologies[J]. Journal of Astronautics,2010,31(3):622-626