Tesis Doctoral
Aircraft trajectory optimization using singular optimal control theory
Autor/es | Franco Espín, Antonio |
Director | Rivas Rivas, Damián
Pérez-Saborid Sánchez-Pastor, Miguel |
Departamento | Universidad de Sevilla. Departamento de Ingeniería Aeroespacial y Mecánica de Fluidos |
Fecha de publicación | 2014 |
Fecha de depósito | 2014-11-27 |
Resumen | The optimization of aircraft trajectories using the theory of singular optimal control is studied in this thesis. To describe the aircraft motion, a general nonlinear 3-degree-of-freedom point-mass model is adopted, along ... The optimization of aircraft trajectories using the theory of singular optimal control is studied in this thesis. To describe the aircraft motion, a general nonlinear 3-degree-of-freedom point-mass model is adopted, along with realistic aerodynamic and pr |
Cita | Franco Espín, A. (2014). Aircraft trajectory optimization using singular optimal control theory. (Tesis Doctoral Inédita). Universidad de Sevilla, Sevilla. |
Ficheros | Tamaño | Formato | Ver | Descripción |
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D_T.PROV48.pdf | 2.377Mb | [PDF] | Ver/ | |