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Títol: Fast Numerical Solvers in Optimal Control for UAV Trajectories

Director/a: Ferrer Ferre, Alex

Email del professor/a: alex.ferrer@upc.edu

Departament del professor/a: 748-FIS

Codirector/a: Betorz Martinez, Francesc

Email del codirector/a: francesc.betorz@upc.edu

Departament del professor/a: 748-FIS

Titulacions:
  • 2010 - GRAU EN ENGINYERIA EN TECNOLOGIES AEROESPACIALS
  • 2010 - GRAU EN ENGINYERIA EN VEHICLES AEROESPACIALS

Identificador de l'oferta: 205-06309

Modalitat: Universitat

Possibilitat de beca/finançament: No

Idioma d'elaboració del treball: Català

Descripció:

This thesis focuses on the development and analysis of fast numerical solvers for solving optimal control problems related to Unmanned Aerial Vehicle (UAV) trajectory planning. The aim is to design algorithms capable of computing time-optimal or energy-efficient UAV trajectories in real time while satisfying dynamic, environmental, and mission constraints.

Objectius:

1. Formulate optimal control problems for UAV trajectory planning considering realistic dynamic constraints; 2. Study existing numerical solvers (direct and indirect methods) and identify performance bottlenecks; 3. Develop fast and robust numerical methods tailored for UAV applications; 4. Compare performance against standard solvers in terms of speed, accuracy, and scalability; 5. Validate the methods on representative UAV trajectory optimization scenarios.

Tasques a realitzar / Característiques:

Tasks: 1. Literature Review: Investigate optimal control theory, UAV dynamics, and state-of-the-art numerical solvers; 2. Problem Modeling: Define UAV trajectory optimization problems with realistic boundary conditions; 3. Solver Development: Implement fast numerical methods (e.g., multiple shooting, collocation, adjoint-based solvers); 4. Performance Optimization: Improve convergence and reduce computational time; 5. Validation: Test the solvers on benchmark UAV scenarios and compare results with standard approaches; 6. Analysis: Evaluate accuracy, robustness, and scalability of the developed methods; 7. Thesis Writing: Compile methodology, experiments, and conclusions.

Tema: ENGINYERIA AERONÀUTICA

Tipus: Estudi

Càrrega de treball:

300 h GRETA - 600 h GREVA

Temàtica ambiental: No

Confidencial (informatiu): No

Ambit de cooperació: No

Publicació: 28/07/2025

Caducitat: 28/07/2026