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Mathematical Problems in Engineering
Volume 2013, Article ID 726945, 11 pages
Research Article

Robust Tracking Control for Rendezvous in Near-Circular Orbits

1Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150001, China
2Department of Engineering, Faculty of Technology and Science, University of Agder, 4898 Grimstad, Norway

Received 1 October 2013; Revised 6 November 2013; Accepted 6 November 2013

Academic Editor: Rongni Yang

Copyright © 2013 Neng Wan et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Citations to this Article [4 citations]

The following is the list of published articles that have cited the current article.

  • Neng Wan, D. Subbaram Naidu, Ming Liu, Ligang Wu, and Weiran Yao, “Adaptive sliding mode control for spacecraft rendezvous in near-circular orbits with time-varying saturation constraint,” 2017 American Control Conference (ACC), pp. 5812–5817, . View at Publisher · View at Google Scholar
  • Neng Wan, Ming Liu, and Hamid Reza Karimi, “Observer-Based Robust Control for Spacecraft Rendezvous with Thrust Saturation,” Abstract and Applied Analysis, vol. 2014, pp. 1–10, 2014. View at Publisher · View at Google Scholar
  • Neng Wan, Mingming Shi, and Weiran Yao, “A Composite Robust Fault-Tolerant Control Scheme for Limited-Thrust Spacecraft Rendezvous in Near-Circular Orbits,” Journal of Dynamic Systems, Measurement and Control, Transactions of the ASME, vol. 139, no. 12, 2017. View at Publisher · View at Google Scholar
  • Neng Wan, Weiran Yao, Xiang Fang, and Yujiong Liu, “Partially independent control scheme for spacecraft rendezvous in near-circular orbits,” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, pp. 095441001877641, 2018. View at Publisher · View at Google Scholar