Journal of Astronomy and Space Sciences

  • 제30권4호
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  • Pages.291-298
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  • 2013
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  • 2093-5587(pISSN)
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  • 2093-1409(eISSN)
한국우주과학회 (The Korean Space Science Society)
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Optimization of Space Debris Collision Avoidance Maneuver for Formation Flying Satellites

  • Seong, Jae-Dong (Department of Satellite Systems and Applications Engineering, University of Science and Technology) ;
  • Kim, Hae-Dong (Department of Satellite Systems and Applications Engineering, University of Science and Technology)
  • 투고 : 2013.10.23
  • 심사 : 2013.11.25
  • 발행 : 2013.12.15
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초록

The concept of the satellite formation flight is area where it is actively study with expandability and safety compare to existing satellite. For execution of duty with more safety issue, it needs to consider hot topic of space debris for operation of formation flight. In this paper, it suggests heuristic algorithm to have avoidance maneuver for space debris towards operating flight formation. Indeed it covers, using common software, operating simulation to nearest space environment and not only to have goal of avoidance but also minimizing the usage of fuel and finding optimization for maximizing cycle of formation flight. For improvement on convergence speed of existing heuristic algorithm, it substitute to hybrid heuristic algorithm, PSOGSA, and the result of simulation, it represents the satisfaction of minimum range for successful avoidance maneuver and compare to not using avoidance maneuver, it keeps more than three times of formation maintenance performance. From these, it is meaningful results of showing several success goals like simple avoidance collision and fuel usage and decreasing number of times of maintaining formation maneuver.

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참고문헌

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