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Collision Avoidance Maneuver Planning Using GA for LEO and GEO Satellite Maintained in Keeping Area

  • Lee, Sang-Cherl (Aerospace Convergence Technology Research Laboratory, Korea Aerospace Research Institute) ;
  • Kim, Hae-Dong (Aerospace Convergence Technology Research Laboratory, Korea Aerospace Research Institute) ;
  • Suk, Jinyoung (Department of Aerospace Engineering, Chungnam National University)
  • Received : 2012.07.11
  • Accepted : 2012.11.20
  • Published : 2012.12.30

Abstract

In this paper, a collision avoidance maneuver was sought for low Earth orbit (LEO) and geostationary Earth orbit (GEO) satellites maintained in a keeping area. A genetic algorithm was used to obtain both the maneuver start time and the delta-V to reduce the probability of collision with uncontrolled space objects or debris. Numerical simulations demonstrated the feasibility of the proposed algorithm for both LEO satellites and GEO satellites.

Keywords

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