Interplanetary low-thrust trajectories optimization using deterministic and stochastic methods

Authors

  • Guilherme Marcos Neves UNESP
  • Denilson Paulo Souza dos Santos UNESP
  • Jorge Kennedy da Silva Formiga UNESP

Abstract

The patched-conic method [2] is fundamental importance in the calculation of interplanetaryorbits in astrodynamics, performing an approach to the orbital dynamics of a spacecraft. [...] 

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References

Englander, J. A. and Conway, B. A. Automated solution of the low-thrust interplanetarytrajectory problem,AIAA Journal of Guidance, Control, and Dynamics, volume 40, pages15-27, 2017. DOI: 10.2514/1.G002124.

Li, J., Zhao, J. and Li, F., A new method of patched-conic for interplanetary orbit,Optik,volume 156, pages 121-127, 2018. DOI: 10.1016/j.ijleo.2017.10.153.

Neves, G. M., dos Santos, D. P., Domingos, R. C., and Formiga, J. K. Orbital maneuversfor asteroids using genetic algorithm,J. Phys.: Conf. Ser., volume 1365, pages 012019, 2019.DOI: 10.1088/1742-6596/1365/1/012019.

Santos, D. P. S. Otimiza ̧c ̃ao de Trajet ́orias Espaciais com Propuls ̃ao El ́etrica Solar e ManobrasGravitacionalmente Assistidas, Tese de Doutorado, INPE, 2009.

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Published

2021-12-20

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Section

Resumos