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Rendezvous missions to temporarily captured near Earth asteroids

  • Published:2016-04 Issue: Volume:123 Page:4-15
  • ISSN:0032-0633
  • Container-title:Planetary and Space Science
  • language:en
  • Short-container-title:Planetary and Space Science

Author:

Brelsford S.,Chyba M.,Haberkorn T.,Patterson G.

Funder

National Science Foundation (NSF)

Division of Mathematical Sciences

Publisher

Elsevier BV

Subject

Space and Planetary Science,Astronomy and Astrophysics

Reference27 articles.

1. Optimal space trajectory design;Besette;Adv. Astronaut. Sci.,2006

2. Minimum fuel control of the planar circular restricted three-body problem;Caillau;Celest. Mech. Dyn. Astronom.,2012

3. Differential continuation for regular optimal control problems;Caillau;Optim. Methods Softw.,2012

4. Designing rendezvous missions with mini-moons using geometric optimal control;Chyba;J. Ind. Manag. Optim.,2014

5. Time-minimal orbital transfers to temporarily-captured natural Earth satellites;Chyba,2014

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