DocumentCode
447452
Title
MER: from landing to six wheels on Mars...twice
Author
Krajewski, Joel ; Burke, Kevin ; Lewicki, Chris ; Limonadi, Daniel ; Trebi-Ollennu, Ashitey ; Voorhees, Chris
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume
2
fYear
2005
fDate
10-12 Oct. 2005
Firstpage
1791
Abstract
Application of the pathfinder landing system design to enclose the much larger Mars Exploration Rover required a variety of rover deployments to achieve the surface driving configuration. The project schedule demanded that software, design, engineering model test, and flight hardware build be accomplished in parallel. This challenge was met through (a) bounding unknown environments against which to design and test, (b) early mechanical prototype testing, (c) constraining the scope of on-board autonomy to survival-critical deployments, (d) executing a balance of nominal and off-nominal test cases, (e) developing off-nominal event mitigation techniques before landing, (f) flexible replanning in response to surprises during operations. Here is discussed several specific events encountered during initial MER surface operations.
Keywords
Mars; aircraft landing guidance; planetary rovers; Mars Exploration Rover; event mitigation technique; mechanical prototype testing; pathfinder landing system design; rover deployment; spacecraft mechanism; surface driving configuration; surface operation; Aerospace engineering; Application software; Design engineering; Hardware; Mars; Prototypes; Software design; Software prototyping; Software testing; Wheels; Airbags; Egress; ITE; MER; Rover Deployments; Spacecraft Mechanisms; Standup; Surface Operations;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems, Man and Cybernetics, 2005 IEEE International Conference on
Print_ISBN
0-7803-9298-1
Type
conf
DOI
10.1109/ICSMC.2005.1571408
Filename
1571408
Link To Document