Comet Thermal Model for Navigation

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

Research output: Contribution to conferencePresentation

Abstract

We implement a numerical model to analyze the thermodynamics that can be used for navigation and orbit determination of future space missions to small bodies. Unlike past models that use a spherical homogeneous model, our model includes the real non-spherical shape of asteroid 433 Eros. The surface temperature map is expressed as a function of latitude and longitude directions for different initial isothermal temperatures. The lack of spherical symmetry is modeled along with the long and short term temperature variations as a consequence of the orbital and spin axis rotations of the body.
Original languageAmerican English
StatePublished - Feb 2013
EventAAS/AIAA Spaceflight Mechanics Meeting - Kauai, HI
Duration: Feb 1 2013 → …

Conference

ConferenceAAS/AIAA Spaceflight Mechanics Meeting
Period2/1/13 → …

Keywords

  • thermodynamics
  • asteroids
  • navigation
  • space missions

Disciplines

  • Aerospace Engineering
  • Navigation, Guidance, Control and Dynamics

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