Fuel optimal low thrust rendezvous with outer planets via gravity assist

Author:

Guo TieDing,Jiang FangHua,Baoyin HeXi,LI JunFeng

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy

Reference27 articles.

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2. Kuninaka H, Nishivama K, Funakai I, et al. Asteroid rendezvous of HAYABUSA explorer using microwave discharge ion engines. In: the 29th International Electric Propulsion Conference. Princeton: Princeton University, 2005

3. Yan C H, McConaghy T T, Chen K J, et al. Preliminary design of nuclear electric propulsion missions to the outer planets. In: AIAA/AAS Astrodynamics Specialist Conference and Exhibit, 16–19, August 2004. Providence, Rhode Island, 2004

4. Hargraves C, Paris S. Direct trajectory optimization using nonlinear programming and collocation. J Guid Control Dyn, 1987, 4: 338–342

5. Enright P J, Conway B A. Discrete approximations to optimal trajectories using direct transcription and nonlinear programming. J Guid Control Dyn, 1992, 4: 994–1002

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