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Analysis of lunar landing simulation results as applied to landing design criteria

机译：应用于着陆设计标准的月球着陆模拟结果分析

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作者
Feiveson, A. H.; Reid, R.;
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年度 1965
页码 1-29
总页数 29
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
LUNAR LANDING; SPACE ENVIRONMENT SIMULATION; SPACECRAFT DESIGN; SPACECRAFT LANDING; STATISTICAL ANALYSIS; CENTER OF GRAVITY; LUNAR MODULE;

机译：LUNaR LaNDING;空间环境模拟;航天器设计;航天飞机着陆;统计分析;重心;登月舱;

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1. Developing Lunar Landing Vehicle Display Requirements Through Content Analysis of Apollo Lunar Landing Voice Communications [J] . Cristin A. Smith a, Mary L. Cummings a, Liang Sim a International Journal of Aviation Psycholohy . 2008,第3期

机译：通过阿波罗登月语音通信的内容分析制定登月车的显示要求
2. Developing Lunar Landing Vehicle Display Requirements Through Content Analysis of Apollo Lunar Landing Voice Communications [J] . Cristin A. Smith, Mary L. Cummings, Liang Sim The international journal of aviation psychology . 2008,第3期

机译：通过阿波罗登月语音通信的内容分析制定登月车的显示要求
3. VISUAL-BASED INTEGRATED NAVIGATION SYSTEM APPLIED TO A SIMULATION OF LUNAR MODULE LANDING [J] . C. T. Kuo, Y. T. Tien, K. W. Chiang International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences . 2020,第4期

机译：基于视觉的集成导航系统应用于月球模块着陆的模拟
4. NEXT LUNAR LANDER: DESCENT AND LANDING GNC ANALYSIS, DESIGN AND SIMULATIONS [C] . D. Neveu, J.-F. Hamel, J. Christy, Annual AAS rocky mountain guidance and control conference . 2010

机译：下一个LUNAR LANDER：下降和降落GNC分析，设计和模拟
5. Time Response Simulation for Nose Landing Gear Shimmy Damper Design [D] . Chen, Yang. 2018

机译：鼻落齿轮散流器设计的时间响应仿真
6. Lower extremity kinematic analysis in male athletes with unilateral anterior cruciate reconstruction in a jump-landing task and its association with return to sport criteria [O] . Sadegh Norouzi, Fateme Esfandiarpour, Sina Mehdizadeh, 2019

机译：男运动员单侧前交叉重建在跳跃着陆任务中的下肢运动学分析及其与恢复运动水平的关系
7. Developing Lunar Landing Vehicle Display Requirements through Content Analysis of Apollo Lunar Landing Voice Communications [O] . Smith C. A., Cummings M. L., Sim L. 2008

机译：通过阿波罗登月语音通信内容分析发展登月车辆显示要求

Analysis of lunar landing simulation results as applied to landing design criteria

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