Arid
DOI10.1016/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
ISSN0094-5765
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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