Effect of Electromagnetic Forces on the Orbital Dynamics of Tethered Satellites-Reference-Cited by-同舟云学术

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Effect of Electromagnetic Forces on the Orbital Dynamics of Tethered Satellites

Published:2005-11 Issue:6 Volume:28 Page:1309-1315
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Lanoix Eric L. M.¹,Misra Arun K.²,Modi Vinod J.³,Tyc George⁴

Affiliation:

1. Titan Corporation, Houston, Texas 77058

2. McGill University, Montreal, Quebec H3A 2K6, Canada

3. University of British Columbia, Vancouver, British Columbia V6T 1Z4, Canada

4. Macdonald Dettweiler Associates, Richmond, British Columbia V6V 2J3, Canada

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/10.2514/1.1759

Reference20 articles.

Cited by 43 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. Introduction;Studies in Systems, Decision and Control;2024

2. Back-stepping sliding mode control for libration control of large swing angles of electrodynamic tether system;Advances in Space Research;2023-07

3. Cross-verification and benchmarking analysis of electrodynamic tether simulators;Acta Astronautica;2023-07

4. Dynamics Analysis of a VLF Linear Antenna in an Anisotropic Magnetoplasma;IEEE Transactions on Antennas and Propagation;2022-11

5. A code for the analysis of missions with electrodynamic tethers;Acta Astronautica;2022-09

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