Collision Avoidance Algorithm for Satellite Formation Reconfiguration under the Linearized Central Gravitational Fields

A collision-free formation reconfiguration trajectory subject to the linearized Hill’s dynamics of relative motion is analytically developed by extending an algorithm for gravity-free space. Based on the initial solution without collision avoidance constraints, the final solution to minimize the d...

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Detalhes bibliográficos

Principais autores:	InYoung Hwang, Sang-Young Park, Chandeok Park
Formato:	Artigo
Idioma:	Inglês
Publicado em:	The Korean Space Science Society 2013-03-01
coleção:	Journal of Astronomy and Space Sciences
Assuntos:	collision avoidance reconfiguration trajectory satellite formation flying
Acesso em linha:	http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2013/v30n1/OJOOBS_2013_v30n1_11.pdf
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