DocumentCode
1879609
Title
Lunar Surface Operation Testbed (LSOT)
Author
Trebi-Ollennu, Ashitey ; Ali, Khaled S. ; Rankin, Arturo L. ; Tso, Kam S. ; Assad, Christopher ; Matthews, Jaret B. ; Deen, Robert G. ; Alexander, Douglass A. ; Toda, Risaku ; Manohara, Harish ; Mojarradi, Mohammad ; Wolf, Michael ; Wright, John R. ; Yen,
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear
2012
fDate
3-10 March 2012
Firstpage
1
Lastpage
16
Abstract
This paper describes a high fidelity mission concept systems testbed at JPL, called Lunar Surface Operations Testbed (LSOT). LSOT provides a unique infrastructure that enables mission concept studies designers to configure and demonstrate end-to-end surface operations using existing JPL mission operations and ground support tools, Lander, robotic arm, stereo cameras, flight software, and soil simulant (regolith), in a high fidelity functional testbed. This paper will describe how LSOT was used to support the MoonRise mission concept study. MoonRise: Lunar South Pole-Aitken Basin Sample Return Mission would place a lander in a broad basin near the moon´s South Pole and return approximately two pounds of lunar materials to Earth for study. MoonRise was one of three candidate missions competing to be selected as the third mission for NASA´s New Frontiers Program of Solar System Explorations. LSOT was used to demonstrate JPL´s extensive experience and understanding of the MoonRise Lander capabilities, design maturity, surface operations systems engineering issues, risks and challenges.
Keywords
lunar surface; robots; space vehicles; JPL mission operations; LSOT; Lunar South Pole-Aitken Basin Sample Return Mission; MoonRise mission; end-to-end surface operations; flight software; lunar surface operation testbed; regolith; robotic arm; soil simulant; stereo cameras; Cameras; Joints; Moon; Robot sensing systems; Software; Substrates;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2012 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4577-0556-4
Type
conf
DOI
10.1109/AERO.2012.6187057
Filename
6187057
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