Flight dynamics results from the OEDIPUS-C tether mission

Author:

Tyc G.1,Vigneron Frank2,Jablonski Alexander2,Han R.3,Modi V.4,Misra A.5

Affiliation:

1. Bristol Aerospace, Ltd., Winnipeg, Canada

2. Canadian Space Agency, St.-Hubert, Canada

3. Manitoba, Univ., Winnipeg, Canada

4. British Columbia, Univ., Vancouver, Canada

5. McGill Univ., Montreal, Canada

Publisher

American Institute of Aeronautics and Astronautics

Cited by 10 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. Survey of Tether System Technology for Space Debris Removal Missions;Journal of Spacecraft and Rockets;2023-09

2. Fault-Tolerant Stabilization of a Tethered Satellite System Using Offset Control;Journal of Spacecraft and Rockets;2008-09

3. Review on Dynamics and Control of Nonelectrodynamic Tethered Satellite Systems;Journal of Spacecraft and Rockets;2006-07

4. On the dynamics of spinning tethered space vehicles;Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences;2001-11-15

5. Nonlinear Dynamics of Two-Body Tethered Satellite Systems: Constant Length Case;The Journal of the Astronautical Sciences;2001-06

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