| Revue: | Journal of the Brazilian Society of Mechanical Sciences and Engineering |
| Base de datos: | PERIÓDICA |
| Número de sistema: | 000312317 |
| ISSN: | 1678-5878 |
| Autores: | Schulz, Walkiria1 Prado, Antonio F.B. Almeida |
| Instituciones: | 1Instituto Nacional de Pesquisas Espaciais, Sao Jose dos Campos, Sao Paulo. Brasil |
| Año: | 2006 |
| Periodo: | Oct-Dic |
| Volumen: | 28 |
| Número: | 4 |
| Paginación: | 375-377 |
| País: | Brasil |
| Idioma: | Inglés |
| Tipo de documento: | Artículo |
| Enfoque: | Experimental |
| Resumen en inglés | 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 |
| Disciplinas: | Ingeniería |
| Palabras clave: | Ingeniería mecánica, Satélites, Astrofísica, Campo de fuerza, Orbita |
| Keyword: | Engineering, Mechanical engineering, Astrophysics, Keplerian Force Field, Force field, Orbit, Satellites |
| Texte intégral: | Texto completo (Ver PDF) |
