| Revista: | Journal of the Brazilian Society of Mechanical Sciences and Engineering |
| Base de datos: | PERIÓDICA |
| Número de sistema: | 000312314 |
| ISSN: | 1678-5878 |
| Autores: | Fernandes, S. da Silva1 Golfetto, W.A2 |
| Instituciones: | 1Instituto Tecnologico de Aeronautica, Departamento de Matematica, Sao Jose dos Campos, Sao Paulo. Brasil 2Centro Tecnico Aeroespacial, Sao Jose dos Campos, Sao Paulo. Brasil |
| Año: | 2005 |
| Periodo: | Abr-Jun |
| Volumen: | 27 |
| Número: | 2 |
| Paginación: | 178-185 |
| País: | Brasil |
| Idioma: | Inglés |
| Tipo de documento: | Artículo |
| Enfoque: | Experimental |
| Resumen en inglés | An algorithm based on gradient techniques, proposed in a companion paper, is applied to numerical analysis of optimal low-thrust limited-power trajectories for simple transfer (no rendezvous) between coplanar circular orbits in a central Newtonian gravity field. The proposed algorithm combines the main positive characteristics of two well-known methods in optimization of trajectories: the steepest-descent method and the direct second variation method. The analysis is carried out for various radius ratios and transfer durations. The results are compared to the ones provided by a linear analytical theory. The performance of the proposed algorithm shows that it is a good tool in determining optimal low-thrust limited-power trajectories between close circular coplanar orbits in a Newtonian central gravity field |
| Disciplinas: | Matemáticas, Ciencia y tecnología, Ingeniería |
| Palabras clave: | Trayectorias espaciales, Algoritmos, Cohetes, Energía, Propulsión |
| Keyword: | Mathematics, Science and technology, Engineering, Propulsion, Space trajectories, Power, Algorithms, Rockets |
| Texto completo: | Texto completo (Ver PDF) |
