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Influence Analysis of Terrain of the Farside of the Moon on Soft-Landing
- LI Fei1, ZHANG He1, WU Xueying1, MA Jinan1, LU Liangliang2
Author information
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1. Institute of Spacecraft System Engineering,Beijing 100094,China;
2. Lunar Exploration and Space Program Center,Beijing 100037,China
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History
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Received |
Revised |
13 Mar 2017 |
28 Mar 2017 |
Issue Date |
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20 May 2022 |
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Chang’e-4 probe is planned to land on the farside of the moon for the first time of the human being. Compared to the nearside of the moon, the terrain on the farside of the moon is rugged and complex, and there is no large flat area, so the change of the terrain will affect the soft-landing of Chang’e-4. The Chang’e-4 landing site on the South-Pole Aitken Basin is analyzed and compared wth the landing area of Chang’e-3 mission, considering the influences ofthe mission design, the lander design and the lunar working procedure. The main conclusions are as follows: 1) The latitude and longitude range of the landing area is reduced from 16.4° and 3° for Chang’e-3 mission to about 4° and 2° for Chang’e-4 mission; 2) During the power descent phase, the strategy after the main deceleration phase is changed from the oblique forward motion trajectory to the vertical down trajectory, and the operation time of the distance measuring sensor is also changed; 3) The signal transmission powers and signal to noise ratios of the microwave ranging and velocity sensor will be improved; 4) The lighting of the lander and the communication by the terrain occlusion will be prediected, and the design operation strategies such as sleep mode or eclipse mode will be established. Through the modification, Chang’e-4 mission can be adapted to the changes in the topography of the farside of the moon to reduce the risk of landing and lunar mission.
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References
[1] 于登云等. 月球软着陆探测器技术[M]. 北京:国防工业出版社,2016.
[2] 褚桂柏,张熇. 月球探测器技术[M]. 北京:中国科学技术出版社,2007.
[3] Sun Z Z,Jia Y,Zhang H. Technological advancements and promotion roles of Chang’e-3 lunar probe mission[J]. Science China (Technological Sciences),2013,43(11):2702-2708
[4] 张健,缪秉魁,廖庆园,等. 月球南极艾特肯盆地的地质特征:探索月球深部的窗口[J]. 矿物岩石地球化学通报,2011年,30(2):234-240.
Zhang J,Miao B K,Liao Q Y,et al. The geological characteristics of the South Pole-Aitken Basin on the Moon:the window to explore the deep composition of the Moon[J]. Bulletin of Mineralogy,Petrology and Geochemistry,2011,30(2):234-240.
[5] Kyeong J K,James M D,Jean P W. The South Pole-Aitken basin region,Moon:GIS-based geologic investigation using Kaguya elemental information[J]. Advances in Space Research,2012,50(12):1629-1637.
[6] David A K,Daniel D D. A global lunar landing site study to provide the scientific context for exploration of the Moon[R]. USA:LPI-JSC Center for Lunar Science and Exploration,2012.
[7] Peterson C A,Hawke B R,Blewett D,et al. Geochemical units on the Moon:The Role of South Pole-Aitken basin[C]//Lunar and Planetary Science XXXIII. USA:[s.n.],2002:46-47.
[8] Peterson C A,Hawke B R,Lucey P G,et al. Anorthosite on the lunar farside and its relationship to South Pole-Aitken Basin[C]//Lunar and Planetary Science XXXI. USA:[s.n.],2000:1680-1681.
[9] Lucey P G,Taylor G J,et al. FeO and TiO2 Concentrations in the South Pole-Aitken Basin:implications for mantle composition and basin formation[J]. Journal of Geophysical Research,1998,103(E2):3701-3708
[10] Wu Y Z,Xue B,Zhao B C,et.al. Global estimates of lunar iron and titanium contents from the Chang’E-1 IIM data [J]. Journal of Geophysical Research:Planets (1991-2012),2012,117(E2):1-23
[11] 李飞,马继楠,张熇,等. 基于月球背面的嫦娥4号着陆区选择方法研究[C]//中国宇航学会深空探测技术专业委员会第十三届学术年会,上海:CDSET-CSA,2016.
[12] 黄翔宇,张洪华,王大轶,等. “嫦娥3号”探测器软着陆自主导航与制导技术[J]. 深空探测学报,2014,1(1):44-51
WANG D Y,LI J,HUANG X Y,et al. A pinpoint autonomous for navigation and hazard avoidance method lunar soft landing[J]. Journal of Deep Space Exploration,2014,1(1):44-51
[13] Klumpp A R. Apollo guidance,navigation and control R-695[R]. [S.l.]:NASA,1971.
[14] Thomas F. Lunar landing and ascent trajectory guidance design for the Autonomous Landing and Hazard Avoidance Technology (ALHAT) Program[J]. Advances in the Astronautical Sciences,2010,136:2317-2336