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Two-impulse, bi-parabolic, and bi-elliptical transfers between coplanar elliptical orbits

  • Published:2020-12 Issue: Volume:177 Page:158-171
  • ISSN:0094-5765
  • Container-title:Acta Astronautica
  • language:en
  • Short-container-title:Acta Astronautica

Author:

Carter ThomasORCID,Humi Mayer

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference27 articles.

1. Die Erreichbarkeit der Himmelskorper, Oldenbourg: Munich, Germany, 1925, The Attainability of Heavenly bodies;Hohmann,1960

2. Note sur la Cinematique generale du mobile dirige;Contensou;Bull. Assoc. Techn., Marit. Aeronaut.,1946

3. Application des methodes de la mecanique du mobile dirige a la theorie du vol plane;Contensou;Bull. Assoc. Techn., Marit. Aeronaut.,1950

4. Minimal rocket trajectories;Lawden;J. Am. Rocket Soc.,1953

5. Stationary rocket trajectories;Lawden;Q. J. Mech.,1954

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Minimum-fuel two-impulse transfer between coplanar noncoaxial elliptical orbits;Advances in Space Research;2024-01

2. Preliminary Design Analysis of Interplanetary Trajectories with Hohmann And Bi-Elliptic Manoeuvres;2023 2nd International Conference on Vision Towards Emerging Trends in Communication and Networking Technologies (ViTECoN);2023-05-05

3. A fast calculation method for asteroid exploration window based on optimal and sub-optimal two-impulse transfer orbits;Acta Astronautica;2021-09

4. Generalized Hohmann, Bi-Parabolic and Bi-Elliptic Planar Impulsive Transfer Using Transformed Variables;Journal of Optimization Theory and Applications;2021-02-12
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