Collocation of geostationary satellites using convex optimization

Frederik J. De Bruijn, Stephan Theil, Daniel Choukroun, Eberhard Gill

Research output: Contribution to journalArticlepeer-review

8 Scopus citations

Abstract

A method is developed to determine station-keeping maneuvers for a fleet of satellites collocated in a geostationary slot. The method is enabled by a linear time-varying formulation of the satellite orbit dynamics in terms of nonsingular orbital elements. A leader-follower control hierarchy is used, such that the motion of the follower satellites is controlled relative to the leader. Key objectives of the station-keeping method are to minimize propellant consumption and to limit the number of maneuvers while guaranteeing safe separation between the satellites. The method is applied in a realistic simulation scenario, including orbit determination, as well as actuation and modeling errors. The method is demonstrated to work for a fleet of four satellites with differences in mass, surface area, and propulsion system for a maneuver cycle of one week. It is then demonstrated that, by reducing the maneuver cycle duration to one day, the method allows collocation of 16 satellites in a single slot, without penalties on propellant consumption.

Original languageEnglish
Pages (from-to)1303-1313
Number of pages11
JournalJournal of Guidance, Control, and Dynamics
Volume39
Issue number6
DOIs
StatePublished - 1 Jan 2016

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