Indirect Optimization of Three-Dimensional Multiple-Impulse Moon-to-Earth Transfers
Author:
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Aerospace Engineering
Link
http://link.springer.com/content/pdf/10.1007/s40295-014-0018-9.pdf
Reference33 articles.
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3. Jones, D.R., Ocampo, C.: Optimization of impulsive trajectories from circular oribt to an excess velocity vector. J. Guid. Control. Dyn. 35(1), 234–244 (2012). doi: 10.2514/1.49237
4. Ocampo, C., Saudemont, R.: Initial trajectory model for a multi- maneuver moon-to-earth abort sequence. J. Guid. Control. Dyn. 33(4), 1184–1194 (2010). doi: 10.2514/1.46955
5. Ocampo, C., Munoz, J.P.: Variational equations for a generalized spacecraft trajectory model. J. Guid. Control. Dyn. 33(5), 1615–1622 (2010). doi: 10.2514/1.46953
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