PhD Thesis
Aircraft trajectory optimization using singular optimal control theory
Author/s | Franco Espín, Antonio |
Director | Rivas Rivas, Damián
Pérez-Saborid Sánchez-Pastor, Miguel |
Department | Universidad de Sevilla. Departamento de Ingeniería Aeroespacial y Mecánica de Fluidos |
Publication Date | 2014 |
Deposit Date | 2014-11-27 |
Abstract | 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 |
Citation | Franco Espín, A. (2014). Aircraft trajectory optimization using singular optimal control theory. (Tesis Doctoral Inédita). Universidad de Sevilla, Sevilla. |
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D_T.PROV48.pdf | 2.377Mb | [PDF] | View/ | |