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  KEYWORD

Nonlinear Model Predictive Control for orbital maneuver in Lunar Orbits

keywords CONTROL SYSTEMS, MODEL PREDICTIVE CONTROL, NONLINEAR SYSTEMS, OPTIMIZATION ALGORITHMS, SIMULATION

Reference persons CARLO NOVARA, MICHELE PAGONE

Thesis type ANALYSIS/SIMULATION

Description The thesis concerns the development of nonlinear guidance and control algorithms - by means of Nonlinear Model Predictive Control - for autonomous space missions. In this scenario, the study of guidance and control systems for autonomous spacecrafts in Lunar orbit is attracting a wide interest among space agencies and companies, in the view of future Lunar missions.
In detail, the thesis will be structured as follows:
- Study of relevant literature on predictive control and lunar orbital maneuvers.
- Development of guidance and control algorithms.
- Study and development of nonlinear optimization algorithm for optimal control.
- High-fidelity simulations for algorithm validation.

Required skills - Advanced automatic control knowledge.
- Matlab/Simulink.
- Optimization algorithm knowledge.

Notes The work will be carried out in cooperation with the University of Pisa.


Deadline 31/12/2022      PROPONI LA TUA CANDIDATURA




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