Optimal low-thrust GTO–GSO transfers using differential evolution
Author:
Publisher
Springer Science and Business Media LLC
Subject
Multidisciplinary
Link
http://link.springer.com/content/pdf/10.1007/s12046-020-01523-x.pdf
Reference8 articles.
1. Gopinath N 2003 Optimal low thrust orbit transfer from GTO to geosynchronous orbit and stationkeeping using electric propulsion system. In: Proceedings of the 54th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law
2. Falck R and Dankanich J 2012 Optimization of low-thrust spiral trajectories by collocation. In: Proceedings of the AIAA/AAS Astrodynamics Specialist Conference, p. 4423
3. Falck R D, Sjauw W K and Smith D A 2014 Comparison of low-thrust control laws for applications in planetocentric space. In: Proceedings of the 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, p. 3714
4. Haberkorn T, Martinon P and Gergaud J 2004 Low thrust minimum-fuel orbital transfer: a homotopic approach. J. Guidance Control Dyn. 27(6): 1046–1060
5. Kirk D E 2012 Optimal control theory: an introduction. Courier Corporation
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