• DocumentCode
    2265832
  • Title

    Concept for coring from a low-mass rover

  • Author

    Backes, Paul ; Khatib, Oussama ; Diaz-Calderon, Antonio ; Warren, James ; Collins, Curtis ; Chang, Zensheu

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
  • fYear
    0
  • fDate
    0-0 0
  • Abstract
    Future Mars missions such as the Mars Sample Return (MSR) mission may benefit from core sample acquisition from a low-mass rover where the rover cannot be assumed to be stationary during a coring operation. Manipulation from Mars rovers is currently done under the assumption that the rover acts as a stationary, stable platform for the arm. An MSR mission scenario with a low-mass rover has been developed and the technology needs have been investigated. Models for alternative types of coring tools and tool-environment interaction have been developed and input along with wheel-soil interaction models into the Stanford Simulation & Active Interfaces (SAI) simulation environment to enable simulation of coring operations from a rover. Coring tests using commercial coring tools indicate that the quality of the core is a critical criterion in the system design. Current results of the models, simulation, and coring tests are provided
  • Keywords
    Mars; aerospace engineering; aerospace robotics; boring; control engineering computing; force control; manipulator dynamics; mobile robots; motion control; planetary rovers; torque control; Mars Sample Return mission; Mars missions; Mars rover manipulation; Stanford Simulation and Active Interfaces; coring operation; low-mass rover; tool-environment interaction; wheel-soil interaction models; Biographies; Computer science; Containers; Contamination; Costs; Laboratories; Mars; Propulsion; Sampling methods; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2006 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    0-7803-9545-X
  • Type

    conf

  • DOI
    10.1109/AERO.2006.1655725
  • Filename
    1655725