Optimal Servicing of Geosynchronous Satellites Academic Article uri icon


  • A method for determining the minimum fuel solution for visiting a set of satellites in a geosynchronous orbit with small inclinations, is presented. Strategies for visiting the satellites include equal time for each visit or equal minimum fuel for the in-plane portion of the maneuver. The minimum fuel solution from this method is found to 25% of the minimum fuel solution for visiting each satellite by proceeding sequentially around the geosynchronous belt. This method is more feasible for servicing a large number of satellites in geosynchronous orbit that have small inclinations.

published proceedings

  • Journal of Guidance, Control, and Dynamics

author list (cited authors)

  • Alfriend, K. T., Lee, D., & Creamer, N. G.

citation count

  • 49

complete list of authors

  • Alfriend, Kyle T||Lee, Deok-Jin||Creamer, N Glenn

publication date

  • January 2006