BRAVE: Bridging the gap between Robust and dAta-driVen control prototypE for launchers

The objective of this activity is to conduct a feasibility study to understand if, and to what extent, sensor-based (i.e. data-driven) control design methods, such as Incremental Nonlinear Dynamic Inversion (INDI), can offer a faster and more robust approach for the prototyping of launcher flight control laws.