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Minimum-time Earth–Moon and Moon–Earth orbital maneuvers using time-domain finite element method

  • Published:2010-02 Issue:3-4 Volume:66 Page:528-538
  • ISSN:0094-5765
  • Container-title:Acta Astronautica
  • language:en
  • Short-container-title:Acta Astronautica

Author:

Fazelzadeh S.A.,Varzandian G.A.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference18 articles.

1. Theorem of image trajectories in the Earth–Moon space;Miele;Acta Astronautica,1960

2. Fundamentals of Astrodynamics;Bate,1971

3. Modern Spacecraft Dynamics and Control;Kaplan,1976

4. Spaceflight Dynamics;Wiesel,1989

5. The Three-body Problem;Marchal,1990

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2. Genetic Algorithm of Energy Consumption Optimization for Reorientation of the Spacecraft Orbital Plane;Mekhatronika, Avtomatizatsiya, Upravlenie;2022-05-06

3. Quaternion Models and Algorithms for Solving the General Problem of Optimal Reorientation of Spacecraft Orbit;Izvestiya of Saratov University. New Series. Series: Mathematics. Mechanics. Informatics;2020

4. Calculating of the Fastest Spacecraft Flights between Circular Orbits;Izvestiya of Saratov University. New Series. Series: Mathematics. Mechanics. Informatics;2017

5. Lunar exploration phase III: Launch window and trajectory design for a lunar lander;Advances in Space Research;2015-09
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