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Aircraft trajectory optimization using singular optimal control theory

 

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Author: Franco Espín, Antonio
Director: Rivas Rivas, Damián
Pérez-Saborid Sánchez-Pastor, Miguel
Department: Universidad de Sevilla. Departamento de Ingeniería Aeroespacial y Mecánica de Fluidos
Date: 2014
Document type: Doctoral Thesis
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 with realistic aerodynamic and pr
Cite: Franco Espín, A. (2014). Aircraft trajectory optimization using singular optimal control theory. (Tesis Doctoral Inédita). Universidad de Sevilla, Sevilla.
Size: 2.377Mb
Format: PDF

URI: http://hdl.handle.net/11441/15236

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