Construction of the Optimal Trajectories for the Earth–Asteroid–Earth Mission under High-Thrust Flight-Reference-Cited by-同舟云学术

Construction of the Optimal Trajectories for the Earth–Asteroid–Earth Mission under High-Thrust Flight

Published:2020-03 Issue:2 Volume:58 Page:111-121
ISSN:0010-9525
Container-title:Cosmic Research
language:en
Short-container-title:Cosmic Res

Author:

Ivashkin V. V.,Lan Anqi

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.1134/S0010952520020057.pdf

Reference30 articles.

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2. Sandford, S.A., The power of sample return missions–Stardust and Hayabusa, Proceedings of the International Astronomical Union Symposium, 2011, vol. 280, pp. 275–287.

3. Ajluni, T., Everett, D., Linn, T., et al., OSIRIS-REx, returning the asteroid sample, 2015 IEEE Aerospace Conference, IEEE, 2015, pp. 1–15.

4. Asteroido-kometnaya opasnost’: vchera, segodnya, zavtra (Asteroid–Comet Hazard: Yesterday, Today, and Tomorrow), Shustov, B.M. and Rykhlova, L.V., Eds., Moscow: Fizmatlit, 2010.

5. Sokolov, L.L., Bashakov, A.A., Borisova, T.P., et al., Impact trajectories of the asteroid Apophis in the 21st century, Sol. Syst. Res., 2012, vol. 46, no. 4, pp. 291–300.

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