Optimal low-thrust rendezvous control.

Author:

EULER EDWARD A.1

Affiliation:

1. Northwestern University, Evanston, III.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 30 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. Optimal Low-Thrust Docking with a Constrained Approach Direction Using Two Intermediate Points;AIAA SCITECH 2024 Forum;2024-01-04

2. Applicability of Clohessy-wiltshire Model For Optimal Low-thrust Rendezvous;Journal of Aerospace Sciences and Technologies;2023-07-29

3. Rendezvous and Docking Simulations Considering J2 Perturbation;Journal of Space Technology and Applications;2022-11

4. Non-iterative angles-only initial relative orbit determination withJ2perturbations;Acta Astronautica;2018-10

5. A Minimum-Fuel Fixed-Time Low-Thrust Rendezvous Solved with the Switching Systems Theory;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2018

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