GN&C Technology Needed to Achieve Pinpoint Landing Accuracy at Mars

机译：GN＆C技术需要在火星上实现精确的着陆精度

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《AIAA Guidance, Navigation, and Control Conference;Applied Aerodynamics Conference and Exhibit;AIAA/AAS Astrodynamics Specialist Conference and Exhibit》|2004年|P.1-12|共12页
会议地点 Providence, RI(US);Providence, RI(US);Providence, RI(US)
作者
T. Brand; L. Fuhrman; D. Geller; P. Hattis; S. Paschall; Y. Tao;
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Charles Stark Draper Laboratory Inc. Cambridge MA;

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机译：使用两个滑动面自主引导的固定时间精确火星着陆
2. Fixed-time pinpoint mars landing using two sliding-surface autonomous guidance [J] . Zhang Yao, Guo Yanning, Ma Guangfu, Acta astronautica . 2019,第Juna期

机译：使用两个滑动表面自主指导的定时定位火星着陆
3. Optical measurement aided autonomous navigation for pinpoint Mars landing [J] . Yan Hong-tao, Dai Ze, Hu Yun-peng, Optik: Zeitschrift fur Licht- und Elektronenoptik: = Journal for Light-and Electronoptic . 2018,第期

机译：用于Pinpoint Mars Landing的光学测量辅助自主导航
4. GNC Technology Needed to Achieve Pinpoint Landing Accuracy at Mars [C] . American Institute of Aeronautics and Astronautics Guidance, Navigation, and Control Conference . 2004

机译：GN＆C技术需要在火星上实现Pinpoint降落精度
5. A Successive Convexification Optimal Guidance Implementation for the Pinpoint Landing of Space Vehicles [D] . Lysandrou, Padraig S. 2020

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6. Preparing for the crewed Mars journey: microbiota dynamics in the confined Mars500 habitat during simulated Mars flight and landing [O] . Petra Schwendner, Alexander Mahnert, Kaisa Koskinen, 2017

机译：为载人火星之旅做准备：模拟火星飞行和着陆过程中密闭的Mars500栖息地中的微生物群落动态
7. An Analysis of Spacecraft Localization from Descent Image Data for Pinpoint Landing on Mars and Other Cratered Bodies [O] . Adnan Ansar, Yang Cheng 2013

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8. Powered Descent Guidance for Mars Pinpoint Landing Based on Model Predictive Control Theory. [R] . Jung, Y., Bang, H. 2016

机译：基于模型预测控制理论的火星定点着陆动力下降制导。

GN&C Technology Needed to Achieve Pinpoint Landing Accuracy at Mars

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