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Collision Avoidance Maneuver Planning Using GA for LEO and GEO Satellite Maintained in Keeping Area
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 Title & Authors
Collision Avoidance Maneuver Planning Using GA for LEO and GEO Satellite Maintained in Keeping Area
Lee, Sang-Cherl; Kim, Hae-Dong; Suk, Jinyoung;
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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.
Geostationary Satellite;Low Earth Orbit Satellite;Collision Avoidance;Genetic Algorithm;Space Debris;Avoidance Maneuver;
 Cited by
상대운동방정식 기반의 우주파편 충돌회피기동의 해석적 설계기법,조동현;김해동;이상철;

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