On the possibility of the guidance of small asteroids to dangerous celestial bodies using the gravity-assist maneuver-Reference-Cited by-同舟云学术

On the possibility of the guidance of small asteroids to dangerous celestial bodies using the gravity-assist maneuver

Published:2013-07 Issue:4 Volume:47 Page:325-333
ISSN:0038-0946
Container-title:Solar System Research
language:en
Short-container-title:Sol Syst Res

Author:

Eismont N. A.,Boyarskii M. N.,Ledkov A. A.,Nazirov R. R.,Dunham D. W.,Shustov B. M.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics

Link

http://link.springer.com/content/pdf/10.1134/S0038094613040102.pdf

Reference10 articles.

1. Brophy, J., Culick, F., Dimotakis, P., and Friedman, L., A safe stepping stone into the solar system, Proc. 63rd Int. Astron. Congr. Naples, Oct. 2012.

2. Eismont, N., Boyarsky, M., Ledkov, A., et al., Using small asteroids to deflect larger dangerous asteroids, Proc. 23rd Int. Symp. on Space Flight Dynamics, Pasadena, 2012. https://issfd.jpl.nasa.gov/home/assets/papers/ISSFD23-IMD2-1.pdf

3. Gooding, R.H., A procedure for solution of Lambert’s orbital boundary-value problem, Celest. Mech. Dyn. Astron., 1990, vol. 48, no. 2, pp. 145–165.

4. JPL Small-Body Browser: 99942 Apophis (2004 MN4). http:/ssd.jpl.nasa.gov/sbdb.cgi?sstr=99942

5. Lancaster, E.R. and Blanchard, R.C., A unified form of Lambert’s theorem, NASA Tech. Note no. TN D-5363, 1969.

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