Analysis of Dynamics and Control During the Deployment of an Annular Tether Group of Spacecraft
Author:
Publisher
Allerton Press
Subject
General Physics and Astronomy,Mechanics of Materials
Link
https://link.springer.com/content/pdf/10.3103/S0025654422601549.pdf
Reference13 articles.
1. V. V. Beletskii and E. M. Levin, Dynamics of Space Tether Systems (Nauka, Moscow, 1990) [in Russian].
2. K. D. Kumar and T. Yasaka, “Rotating formation flying of three satellites using tethers,” J. Spacecr. 41 (6), 973–985 (2004). https://doi.org/10.2514/1.14251
3. M. Kim and C. D. Hall, “Control of a rotating variable-length tethered system,” J. Guid. Contr. Dyn. 27 (5), 849–858 (2004). https://doi.org/10.2514/1.3226
4. P. Williams, “Optimal deployment/retrieval of a tethered formation spinning in the orbital plane,” J. Spacecr. 43 (3), 638–650 (2006). https://doi.org/10.2514/1.17093
5. B. Su, F. Zhang, and P. Huang, “Robust control of triangular tethered satellite formation with unmeasured velocities,” Acta Astronaut. 186, 190–202 (2021). https://doi.org/10.1016/j.actaastro.2021.04.045
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