Riemannian metric of the averaged energy minimization problem in orbital transfer with low thrust
Author:
Affiliation:
1. Institut de Mathématiques de Bourgogne, 9, avenue Savary, 21078 Dijon, France
2. ENSEEIHT-IRIT, UMR CNRS 5505, 2, rue Camichel, 31071 Toulouse, France
Publisher
European Mathematical Society - EMS - Publishing House GmbH
Subject
Mathematical Physics,Analysis,Applied Mathematics
Cited by 13 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. On the convergence of time-optimal maneuvers of fast-oscillating control systems;2021 European Control Conference (ECC);2021-06-29
2. Quasi-time-optimal steering law for low-thrust orbit transfer considering angular momentum and torque constraints;Acta Astronautica;2021-05
3. Minimum energy coplanar orbit transfer of geostationary spacecraft using time-averaged Hamiltonian;Acta Astronautica;2019-07
4. Near Time-Minimal Earth to L1 Transfers for Low-Thrust Spacecraft;Journal of Guidance, Control, and Dynamics;2017-11
5. Lunar Perturbation of the Metric Associated to the Averaged Orbital Transfer;Springer INdAM Series;2015
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