한국항공우주학회지 (Journal of the Korean Society for Aeronautical & Space Sciences)

  • 제38권2호
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  • Pages.141-149
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  • 2010
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  • 1225-1348(pISSN)
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  • 2287-6871(eISSN)
한국항공우주학회 (The Korean Society for Aeronautical and Space Sciences)
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연료 균형을 고려한 인공위성 편대비행유지 최적 임펄스 제어

Optimal Impulsive Maneuver for Satellite FormationKeeping with Fuel Balancing

  • 목성훈 (KAIST 항공우주공학전공 대학원) ;
  • 최윤혁 (KAIST 항공우주공학전공 대학원) ;
  • 조동현 (KAIST 인공위성연구센터) ;
  • 방효충 (KAIST 항공우주공학)
  • 투고 : 2009.10.27
  • 심사 : 2010.01.27
  • 발행 : 2010.02.01
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초록

위성 편대 비행 시 주위성과 부위성 간의 연료 소비 균형을 고려한 임펄스 기동에 관한 연구를 수행하였다. 위성 간 사용가능한 연료량을 비교하여 가중치(weight)를 두고 가격함수(cost function)를 설계하여 라그랑지 승수법을 통해 필요한 임펄스를 획득하였다. 상대궤도 발산 방지를 위해 에너지 매칭 기법을 사용하였고, 임펄스 기동 후 상대 거리 구속이 이루어짐을 시뮬레이션을 통해 확인하였다. 시뮬레이션은 지구 중력 외의 외란이 없는 경우와 대기 항력이 외란으로 존재하는 상황으로 시나리오를 나누어 수행하였다. 본 논문 결과는 이후 실제로 위성을 편대로 사용한 위성 군집 비행 시, 상대 궤도 구속 요건을 만족하고 각 위성의 연료량을 비교한 임펄스 기동이 요구될 때 사용가능할 것으로 기대된다.

This paper contains impulsive maneuver which considers fuel consumption balance of chief satellite and deputy satellite in satellite formation flying. Thrust input is obtained by Lagrange' Multiplier method which is constructed by cost function with weight parameter of each satellite. Energy matching constraint is applied for boundedness of relative orbit, and theoretical solutions are verified by simulation results. Simulations are divided into two scenarios, with or without air-drag effect. This paper's results are expected to be used in real satellite formation flying, when fuel-balancing impulsive maneuver for relative orbit boundedness is needed.

키워드

참고문헌

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