Periodic Orbits and Equilibria Near Jovian Moons Using an Electrodynamic Tether-Reference-Cited by-同舟云学术

Periodic Orbits and Equilibria Near Jovian Moons Using an Electrodynamic Tether

Published:2015-01 Issue:1 Volume:38 Page:15-29
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Bokelmann Kevin A.¹,Russell Ryan P.¹,Lantoine Gregory²

Affiliation:

1. Aerospace and Engineering Mechanics, University of Texas at Austin, Austin, Texas 78712

2. Mission Design and Navigation Section, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109-8099

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.G000428

Reference31 articles.

1. Committee on the Planetary Science Decadal Survey, “Vision and Voyages for Planetary Science in the Decade 2013-2022,” National Research Council of the National Academies, National Academy Press, Washington, D.C. (to be published).

2. Bare wire anodes for electrodynamic tethers

3. Systems analysis of electrodynamic tethers

4. Io Exploration with Electrodynamic Tethers

5. Electrodynamic Tether at Jupiter—II: Fast Moon Tour After Capture

Cited by 5 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. Review of Trajectory Design and Optimization for Jovian System Exploration;Space: Science & Technology;2023-01

2. A mathematical study of the tethered slingshot maneuver using the elliptic restricted problem;Nonlinear Dynamics;2020-10-08

3. Trajectory Design Leveraging Low-Thrust, Multi-Body Equilibria and their Manifolds;The Journal of the Astronautical Sciences;2020-04-14

4. Magnetour: Surfing planetary systems on electromagnetic and multi-body gravity fields;Acta Astronautica;2017-09

5. Jovian Orbit Capture and Eccentricity Reduction Using Electrodynamic Tether Propulsion;Journal of Spacecraft and Rockets;2015-03