Orbital Evolution and Environmental Analysis Around Asteroid 2008 EV5

Pedro J. Llanos, James K. Miller, Gerald R. Hintz, Pedro J Llanos de la Concha

Research output: Contribution to conferencePresentation

Abstract

The orbital evolution and environmental analyses around the target asteroid, 2008 EV5, for the ESA’s Marco Polo R mission are assessed during the proximity operations to minimize the efforts towards the improvement of the Guidance, Navigation and Control system. With this analysis, we will extend our knowledge in the decision-making when the spacecraft is flying under unknown environmental conditions, such as the solar radiation pressure and the gravitational harmonics due to the irregular shape of the body. We compare analyses performed on different asteroid shape models, such as a parameterized model, an ellipsoid model and a high fidelity mascons shape model.
Original languageAmerican English
StatePublished - Jan 2014
EventAAS/AIAA Spaceflight Mechanics Meeting - Napa, CA
Duration: Feb 1 2016 → …

Conference

ConferenceAAS/AIAA Spaceflight Mechanics Meeting
Period2/1/16 → …

Keywords

  • spacecraft navigation
  • Asteroid 2008 EV5
  • Marco Polo R mission
  • solar radiation pressure

Disciplines

  • Aerospace Engineering
  • Space Vehicles

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