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Design and optimization of low-thrust orbital phasing maneuver

  • Published:2015-04 Issue: Volume:42 Page:365-375
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Shang Haibin,Wang Shuai,Wu Weiren

Funder

National Basic Research Program of China

National Science Foundation of China

Research Fund for the Doctoral Program of Higher Education of China

Excellent Young Scholars Research Fund of Beijing Institute of Technology

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference16 articles.

1. Very low-thrust trajectory optimization using a direct SQP method;Betts;J. Comput. Appl. Math.,2000

2. Improved Edelbaum's approach to optimize low Earth/geostationary orbits low-thrust transfers;Casalino;J. Guid. Control Dyn.,2007

3. Semi-analytical solution for the optimal low-thrust deflection of near-earth objects;Colombo;J. Guid. Control Dyn.,2009

4. Propulsion requirements for controllable satellites;Edelbaum;J. Am. Rocket Soc.,1961

5. Analytic orbital averaging technique for computing tangential-thrust trajectories;Gao;J. Guid. Control Dyn.,2005

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