Asteroid deflection with safe harbors found via numerical optimization

Bruce A. Conway, Siegfried Eggl, Daniel Hestroffer

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

If it were feasible, given the warning time of an actual hazardous asteroid approach, to conduct the deflection in such a way as to place the asteroid in a region of phase space that does not yield a significant future impact risk (i.e. a "safe harbor") with the Earth, this should certainly be done. In this work a numerical method is used to optimize all of the relevant mission parameters for a spacecraft to deflect an asteroid via impact. The objective of the numerical optimizer is to maximize the initial deflection obtained while assuring that subsequent close approach distances of the asteroid to the Earth are only increased by the initial deflection.

Original languageEnglish (US)
Title of host publicationSpaceflight Mechanics 2017
EditorsJon A. Sims, Frederick A. Leve, Jay W. McMahon, Yanping Guo
PublisherUnivelt Inc.
Pages565-575
Number of pages11
ISBN (Print)9780877036371
StatePublished - 2017
Event27th AAS/AIAA Space Flight Mechanics Meeting, 2017 - San Antonio, United States
Duration: Feb 5 2017Feb 9 2017

Publication series

NameAdvances in the Astronautical Sciences
Volume160
ISSN (Print)0065-3438

Other

Other27th AAS/AIAA Space Flight Mechanics Meeting, 2017
CountryUnited States
CitySan Antonio
Period2/5/172/9/17

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

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