Indirect Optimization of Robust Orbit Transfer Considering Thruster Underperformance
Data Reduction for Optimizing the Attitude Control Dispatch in a Spacecraft
Evolutionary Optimisation of a Flexible-Launcher Simple Adaptive Control System
Near-Optimal Guidance and Pulse-Modulated Reduced-Attitude Control for Orbit Injection
Advances in the Control Propellant Minimization for the Next Generation Gravity Mission
Second-order Sufficient Conditions of Strong Minimality with applications to Orbital Transfers
The ERC-Funded EXTREMA Project: Achieving Self-Driving Interplanetary CubeSats
A Pareto Front Numerical Reconstruction Strategy Applied to a Satellite System Conceptual Design