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International Journal of Aerospace Engineering
Volume 2012, Article ID 152683, 14 pages
http://dx.doi.org/10.1155/2012/152683
Research Article

Indirect Optimization of Satellite Deployment into a Highly Elliptic Orbit

1Dipartimento di Ingegneria Meccanica e Aerospaziale, Politecnico di Torino, Corso Duca degli Abruzzi 24, 10129 Torino, Italy
2Dipartimento di Ingegneria Meccanica e Aerospaziale, Sapienza Università di Roma, Via Eudossiana 18, 00184 Roma, Italy

Received 1 November 2011; Revised 1 March 2012; Accepted 19 March 2012

Academic Editor: C. B. Allen

Copyright © 2012 Francesco Simeoni 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 [5 citations]

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

  • Francesco Simeoni, Lorenzo Casalino, Alessandro Zavoli, and Guido Colasurdo, “Deployment of a Two-Spacecraft Formation into a Highly Elliptic Orbit with Collision Avoidance,” AIAA/AAS Astrodynamics Specialist Conference, . View at Publisher · View at Google Scholar
  • Alessandro Zavoli, and Guido Colasurdo, “Indirect Optimization of Finite-Thrust Cooperative Rendezvous,” Journal of Guidance, Control, and Dynamics, pp. 1–11, 2014. View at Publisher · View at Google Scholar
  • Lorenzo Casalino, and Guido Colasurdo, “Tentative solutions for indirect optimization of spacecraft trajectories,” Springer Optimization and Its Applications, vol. 114, pp. 87–102, 2016. View at Publisher · View at Google Scholar
  • Yue You, Hua Wang, Christophe Paccolat, Volker Gass, Jean-Philippe Thiran, and Jiu Ren Li, “Time and Covariance Threshold Triggered Optimal Uncooperative Rendezvous Using Angles-Only Navigation,” International Journal of Aerospace Engineering, vol. 2017, pp. 1–10, 2017. View at Publisher · View at Google Scholar
  • Yunfeng Dong, Xiaona Wei, Lu Tian, Fengrui Liu, and Guangde Xu, “A Novel Double Cluster and Principal Component Analysis-Based Optimization Method for the Orbit Design of Earth Observation Satellites,” International Journal of Aerospace Engineering, vol. 2017, pp. 1–15, 2017. View at Publisher · View at Google Scholar