Low-Thrust Many-Revolution Trajectory Optimization via Differential Dynamic Programming and a Sundman Transformation
Author:
Funder
NASA Space Technology Research Fellowship
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Aerospace Engineering
Link
http://link.springer.com/article/10.1007/s40295-017-0122-8/fulltext.html
Reference38 articles.
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4. Edelbaum, T.N.: Optimum low-thrust rendezvous and station keeping. AIAA J. 2(7), 1196–1201 (1964)
5. Kéchichian, J.A.: Optimal low-thrust rendezvous using equinoctial orbit elements. Acta Astronaut. 38(1), 1–14 (1996)
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