Necessary condition for temporary asteroid capture
Author:
Affiliation:
1. Department of Aviation Engineering, College of Aviation, Inner Mongolia University of Technology , Hohhot 010051 , China
2. Department of Mechanics, College of Science, Inner Mongolia University of Technology , Hohhot 010051 , China
Abstract
Publisher
Walter de Gruyter GmbH
Subject
Space and Planetary Science,Astronomy and Astrophysics
Link
https://www.degruyter.com/document/doi/10.1515/astro-2022-0222/pdf
Reference16 articles.
1. Anderson BD, Lo M. 2018. Dynamics of asteroid 2006 RH120: Temporary capture phase. 2018 Space Flight Mechanics Meeting. 2018 Jan 8–12; Kissimmee (FL), USA. AIAA, 2018. p. 1689.
2. Baoyin HX, Chen Y, Li JF. 2010. Capturing near earth objects. Res Astron Astrophys. 10(6):587.
3. Bolin B, Jedicke R, Granvik M, Brown P, Howell E, Nolan MC, et al. 2014. Detecting Earth’s temporarily-captured natural satellites – Minimoons. Icarus. 241:280–297.
4. Ceriotti M, Sanchez JP. 2016. Control of asteroid retrieval trajectories to libration point orbits. Acta Astronaut. 126:342–353.
5. Chyba M, Granvik M, Jedicke R, Patterson G, Picot G, Vaubaillon J. 2014. Time-minimal orbital transfers to temporarily-captured natural Earth satellites. Optimization and Control Techniques and Applications. Berlin, Heidelberg: Springer. p. 213–235.
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