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Mars Tumbleweed Simulation Using Singular Perturbation TheoryThe Mars Tumbleweed is a new surface rover concept that utilizes Martian winds as the primary source of mobility. Several designs have been proposed for the Mars Tumbleweed, all using aerodynamic drag to generate force for traveling about the surface. The Mars Tumbleweed, in its deployed configuration, must be large and lightweight to provide the ratio of drag force to rolling resistance necessary to initiate motion from the Martian surface. This paper discusses the dynamic simulation details of a candidate Tumbleweed design. The dynamic simulation model must properly evaluate and characterize the motion of the tumbleweed rover to support proper selection of system design parameters. Several factors, such as model flexibility, simulation run times, and model accuracy needed to be considered in modeling assumptions. The simulation was required to address the flexibility of the rover and its interaction with the ground, and properly evaluate its mobility. Proper assumptions needed to be made such that the simulated dynamic motion is accurate and realistic while not overly burdened by long simulation run times. This paper also shows results that provided reasonable correlation between the simulation and a drop/roll test of a tumbleweed prototype.
Document ID
20050207367
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Raiszadeh, Behzad
(NASA Langley Research Center Hampton, VA, United States)
Calhoun, Phillip
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
AIAA Paper 2005-6423
Report Number: AIAA Paper 2005-6423
Meeting Information
Meeting: AIAA Modeling and Simulation Technologies Conference and Exhibit
Location: San Francisco, CA
Country: United States
Start Date: August 15, 2005
End Date: August 18, 2005
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
OTHER: 23-062-10-ED
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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