DocumentCode :
3200451
Title :
The Phoenix Mars Lander Robotic Arm
Author :
Bonitz, Robert ; Shiraishi, Lori ; Robinson, Matthew ; Carsten, Joseph ; Volpe, Richard ; Trebi-Ollennu, Ashitey ; Arvidson, Raymond E. ; Chu, P.C. ; Wilson, J.J. ; Davis, K.R.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
fYear :
2009
fDate :
7-14 March 2009
Firstpage :
1
Lastpage :
12
Abstract :
The Phoenix Mars Lander Robotic Arm (RA) has operated for 149 sols since the Lander touched down on the north polar region of Mars on May 25, 2008. During its mission it has dug numerous trenches in the Martian regolith, acquired samples of Martian dry and icy soil, and delivered them to the Thermal Evolved Gas Analyzer (TEGA) and the Microscopy, Electrochemistry, and Conductivity Analyzer (MECA). The RA inserted the Thermal and Electrical Conductivity Probe (TECP) into the Martian regolith and positioned it at various heights above the surface for relative humidity measurements. The RA was used to point the Robotic Arm Camera to take images of the surface, trenches, samples within the scoop, and other objects of scientific interest within its workspace. Data from the RA sensors during trenching, scraping, and trench cave-in experiments have been used to infer mechanical properties of the Martian soil. This paper describes the design and operations of the RA as a critical component of the Phoenix Mars Lander necessary to achieve the scientific goals of the mission.
Keywords :
Mars; aerospace robotics; mobile robots; planetary rovers; robot vision; Martian regolith; Phoenix Mars lander robotic arm; conductivity analyzer; electrochemistry; north polar region; robotic arm camera; thermal evolved gas analyzer; Cameras; Humidity measurement; Mars; Mechanical sensors; Microscopy; Probes; Robot sensing systems; Robot vision systems; Soil; Thermal conductivity;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace conference, 2009 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-2621-8
Electronic_ISBN :
978-1-4244-2622-5
Type :
conf
DOI :
10.1109/AERO.2009.4839306
Filename :
4839306
Link To Document :
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