Artículo

Optimal space maneuvers in three dimensions

Schulz, WalkiriaIcon ; Almeida Prado, Antônio F. B.
Fecha de publicación: 10/2006
Editorial: Brazilian Society of Mechanical Sciences & Engineering
Revista: Journal of the Brazilian Society of Mechanical Sciences and Engineering
ISSN: 1678-5878
e-ISSN: 1806-3691
Idioma: Inglés
Tipo de recurso: Artículo publicado
Clasificación temática:

Resumen

The objective of this paper is to study the problem of orbital maneuvers for an artificial satellite moving in a Keplerian Force Field. Analytical equations are derived to solve this problem. Several cases are studied to validate the algorithm developed. The results show that the theory developed here are suitable for real simulations and mission analysis.
Palabras clave: Artificial Satellites , Orbital Maneuvers , 3D , Optimization
 
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info:eu-repo/semantics/openAccess Excepto donde se diga explícitamente, este item se publica bajo la siguiente descripción: Creative Commons Attribution-NonCommercial 2.5 Unported (CC BY-NC 2.5)
Identificadores
URI: http://hdl.handle.net/11336/247138
URL: https://www.scielo.br/j/jbsmse/a/V48Y8fG5bSbFqYb6tDjqR7R/?lang=en
DOI: https://doi.org/10.1590/S1678-58782006000400001
Colecciones
Articulos(CCT - CORDOBA)
Articulos de CTRO.CIENTIFICO TECNOL.CONICET - CORDOBA
Citación
Schulz, Walkiria; Almeida Prado, Antônio F. B.; Optimal space maneuvers in three dimensions; Brazilian Society of Mechanical Sciences & Engineering; Journal of the Brazilian Society of Mechanical Sciences and Engineering; 28; 4; 10-2006; 375-377
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