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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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 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
Geostationary Satellite;Low Earth Orbit Satellite;Collision Avoidance;Genetic Algorithm;Space Debris;Avoidance Maneuver;
 Language
English
 Cited by
1.
상대운동방정식 기반의 우주파편 충돌회피기동의 해석적 설계기법,조동현;김해동;이상철;

제어로봇시스템학회논문지, 2013. vol.19. 11, pp.1048-1052 crossref(new window)
1.
Analytical Design of the Space Debris Collision Avoidance Maneuver based on Relative Dynamics, Journal of Institute of Control, Robotics and Systems, 2013, 19, 11, 1048  crossref(new windwow)
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