Optimal Oscillation Suppression Control for Tether Sling-Shot System
Author:
Affiliation:
1. Department of Aerospace Engineering, Tokyo Metropolitan University
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tastj/15/0/15_TJSAS-D-17-00022/_pdf
Reference12 articles.
1. 1) Carroll, J. A.: Tether Applications in Space Transportation, Acta Astronautica,13 (1986), pp. 165–174.
2. 2) Cartmell, M. P.: Generating Velocity Increments by Means of a Spinning Motorized Tether, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Joint Propulsion Conferences, 1998, pp.1–12.
3. 3) Zieger, S. W. and Cartmell, M. P.: Using Motorized Tethers for Payload Orbital Transfer, J. Spacecraft Rockets, 38 (2001), pp.904–913.
4. 4) Qi, N., Yang, Y., Wei, C., and Zhao, J.: Two-Dimensional Dynamicsof a New Configuration of Continuous Cislunar Payloads Transfer System, Trans. Jpn. Soc. Aeronaut. Space Sci., 59 (2016), pp. 71–80.
5. 5) Chen, Y. and Cartmell, M. P.: Hybrid Fuzzy Sliding Mode Control for Motorized Space Tether Spin-up When Coupled with Axial and Torsional Oscillation, Astrophys. Space Sci., 326 (2010), pp.105–118.
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