Planar Problem of an Optimal Transfer of a Low-Thrust Spacecraft from High-Elliptic to Geosynchronous Orbit

Author:

Akhmetshin R. Z.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Cited by 8 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. Application of the complex-dual algebra for solving the optimization problem of perturbed low-thrust trajectories;XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION;2023

2. Typical Cases of Singular Points in Low-Thrust Mission Optimization;Cosmic Research;2022-04

3. Optimization of Perturbed Spacecraft Trajectories Using Complex Dual Numbers. Part 1: Theory and Method;Cosmic Research;2021-09

4. Optimization of Multi-revolution Limited Power Trajectories Using Angular Independent Variable;Journal of Optimization Theory and Applications;2021-04-28

5. Optimization of finite-thrust trajectories with fixed angular distance;Acta Astronautica;2021-04

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