| Revista: | Journal of the Brazilian Society of Mechanical Sciences |
| Base de datos: | PERIÓDICA |
| Número de sistema: | 000312023 |
| ISSN: | 0100-7386 |
| Autores: | Oliva, P1 Leite-Filho, W.C |
| Instituciones: | 1Instituto de Aeronautica e Espaco, Divisao de Sistemas Espaciais, Sao Jose dos Campos, Sao Paulo. Brasil |
| Año: | 2000 |
| Volumen: | 22 |
| Número: | 2 |
| Paginación: | 149-168 |
| País: | Brasil |
| Idioma: | Inglés |
| Tipo de documento: | Artículo |
| Enfoque: | Analítico |
| Resumen en inglés | A control law was designed for a satellite launcher ( rocket ) vehicle using eigenstructure assignment in order that the vehicle tracks a reference attitude and also to decouple the yaw response from roll and pitch manoeuvres and to decouple the pitch response from roll and yaw manoeuvres. The design was based on a complete linear coupled model obtained from the complete vehicle non linear model by linearization at each trajectory point. After all, the design was assessed with the vehicle time varying non-linear model showing a good performance and robustness. The used design method is explained and a case study for the Brazilian satellite launcher ( VLS Rocket ) is reported |
| Disciplinas: | Ingeniería, Matemáticas |
| Palabras clave: | Ingeniería de transportes, Matemáticas aplicadas, Cohetes, Rastreo, Control, Desacoplamiento, Eigenestructuras |
| Keyword: | Engineering, Mathematics, Transportation engineering, Applied mathematics, Rockets, Tracking, Control, Decoupling, Eigenstructures |
| Texto completo: | Texto completo (Ver HTML) |
