Optimal low-thrust rendezvous control.
Author:
Affiliation:
1. Northwestern University, Evanston, III.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5287
Reference18 articles.
1. Terminal Guidance System for Satellite Rendezvous
2. SECOND APPROXIMATION TO THE SOLUTION OF THE RENDEZVOUS EQUATIONS
3. Rendezvous Problem for Nearly Circular Orbits
4. Second-order solution to the elliptical rendezvous problem.
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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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