Thesis

Thesis projects are available in the areas of astrodynamics, optimal control, and autonomous aerospace systems.

All projects involve mathematical modeling, numerical simulation, and algorithm development.

📩 To apply, send an email to alessandro.zavoli@uniroma1.it including your CV or Exam list and a short statement of interests (5–10 lines).

AVAILABLE THESES

Earth–Moon Transfers in the Bi-Circular 4-Body Problem

This theis focuses on the design and optimization of low-energy Earth–Moon transfer trajectories within the Bi-Circular 4-Body Problem framework (Earth–Moon–Sun system).

modeling of multi-body dynamical systems
design of low-energy / ballistic capture trajectories
numerical optimization and analysis

Theses

Theses are available on all research topics. Tutors are available on selected topics:

Indirect optimization of interplanetary missions
Tutor:
Autonomous Upper Stage Guidance Using Convex Optimization and Model Predictive Control
Tutor: Boris Benedikter
Multi-target trajectory optimization: active debris removal
Tutor: Lorenzo Federici
Reinforcement Learning for low-thrust interplanetary mission design
Tutor: Lorenzo Federici
Robust attitude control of launch vehicle in atmospheric flight
Tutor: Vincenzo D'Antuono
Post-Flight trajectory recostruction & thrust performance identification
Tutor: Vincenzo D'Antuono

Currently assigned / past theses

Master

Structured H∞ Control for a Flexible Launch Vehicle
Indirect methods for designing many-revolution trajectories and applications to dwarf planet missions
Indirect Optimization of an interplanetary mission to Ceres

Bachelor

Algoritmi genetici ed applicazioni in ambito aerospaziale
Particle swarm optimization per applicazioni aerospaziali
L'algoritmo CMA-ES pert l'ottimizzazione di traiettorie impulsive
Active debris removal missions
Ottimizzazione mediante ACO e applicazioni spaziali

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