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DOI | 10.1016/j.actaastro.2012.02.022 |
Evaluation of dual multi-mission space exploration vehicle operations during simulated planetary surface exploration | |
Abercromby, Andrew F. J.1; Gernhardt, Michael L.2; Jadwick, Jennifer1 | |
通讯作者 | Abercromby, Andrew F. J. |
来源期刊 | ACTA ASTRONAUTICA
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ISSN | 0094-5765 |
出版年 | 2013 |
卷号 | 90期号:2页码:203-214 |
英文摘要 | Introduction: A pair of small pressurized rovers (multi-mission space exploration vehicles, or MMSEVs) is at the center of the Global Point-of-Departure architecture for future human lunar exploration. Simultaneous operation of multiple crewed surface assets should maximize productive crew time, minimize overhead, and preserve contingency return paths. Methods: A 14-day mission simulation was conducted in the Arizona desert as part of NASA’s 2010 Desert Research and Technology Studies (DRATS) field test. The simulation involved two MMSEV earth-gravity prototypes performing geological exploration under varied operational modes affecting both the extent to which the MMSEVs must maintain real-time communications with the mission control center (Continuous [CC] versus Twice-a-Day [2/D]) and their proximity to each other (Lead-and-Follow [L&F] versus Divide-and-Conquer [D&C]). As part of a minimalist lunar architecture, no communication relay satellites were assumed. Two-person crews (an astronaut and a field geologist) operated each MMSEV, day and night, throughout the entire 14-day mission, only leaving via the suit ports to perform simulated extravehicular activities. Metrics and qualitative observations enabled evaluation of the extent to which the operating modes affected productivity and scientific data quality (SDQ). Results and discussion: SDQ was greater during CC mode than during 2/D mode; metrics showed a marginal increase while qualitative assessments suggested a practically significant difference. For the communications architecture evaluated, significantly more crew time (14% per day) was required to maintain communications during D&C than during L&F (5%) or 2/D (2%), increasing the time required to complete all traverse objectives. Situational awareness of the other vehicle’s location, activities, and contingency return constraints were qualitatively enhanced during L&F and 2/D modes due to line-of-sight and direct MMSEV-to-MMSEV communication. Future testing will evaluate approaches to operating without real-time space-to-earth communications and will include quantitative evaluation and comparison of the efficacy of mission operations, science operations, and public outreach operations. (C) 2012 IAA. Published by Elsevier Ltd. All rights reserved. |
英文关键词 | MMSEV Rover Exploration Lunar Analog Simulation |
类型 | Article |
语种 | 英语 |
国家 | USA |
收录类别 | SCI-E |
WOS记录号 | WOS:000322561100003 |
WOS类目 | Engineering, Aerospace |
WOS研究方向 | Engineering |
资源类型 | 期刊论文 |
条目标识符 | http://119.78.100.177/qdio/handle/2XILL650/175414 |
作者单位 | 1.Wyle Integrated Sci & Engn Grp, Houston, TX USA; 2.NASA, Lyndon B Johnson Space Ctr, Houston, TX 77058 USA |
推荐引用方式 GB/T 7714 | Abercromby, Andrew F. J.,Gernhardt, Michael L.,Jadwick, Jennifer. Evaluation of dual multi-mission space exploration vehicle operations during simulated planetary surface exploration[J],2013,90(2):203-214. |
APA | Abercromby, Andrew F. J.,Gernhardt, Michael L.,&Jadwick, Jennifer.(2013).Evaluation of dual multi-mission space exploration vehicle operations during simulated planetary surface exploration.ACTA ASTRONAUTICA,90(2),203-214. |
MLA | Abercromby, Andrew F. J.,et al."Evaluation of dual multi-mission space exploration vehicle operations during simulated planetary surface exploration".ACTA ASTRONAUTICA 90.2(2013):203-214. |
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