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Modeling and Simulation of Asteroid Capture Using a Deformable Membrane Capture Device

[+] Author Affiliations
Håvard Fjær Grip, Miguel San Martin, Abhinandan Jain, Bob Balaram, Jonathan Cameron, Steven Myint

California Institute of Technology, Pasadena, CA

Paper No. DETC2015-47840, pp. V006T10A036; 10 pages
doi:10.1115/DETC2015-47840
From:
  • ASME 2015 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference
  • Volume 6: 11th International Conference on Multibody Systems, Nonlinear Dynamics, and Control
  • Boston, Massachusetts, USA, August 2–5, 2015
  • Conference Sponsors: Design Engineering Division, Computers and Information in Engineering Division
  • ISBN: 978-0-7918-5716-8
  • Copyright © 2015 by ASME

abstract

The National Aeronautics and Space Administration have recently been investigating a mission concept known as the Asteroid Redirect Mission, aimed at collecting a large amount of asteroid material and transporting it into lunar orbit for inspection by human astronauts. Of the two mission options that have been considered, one involves the capture of an entire near-Earth asteroid in the 10-m class by a robotic spacecraft. The spacecraft would first make contact with the asteroid through a deformable membrane, before securing it inside a large flexible bagging mechanism. In this paper we describe the development and implementation of a model designed for simulation of the capture process, which includes a low-complexity representation of the interaction dynamics.

Copyright © 2015 by ASME

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