Optimized Packings in Space Engineering Applications: Part I
Second-order Sufficient Conditions of Strong Minimality with applications to Orbital Transfers
Choice of the Optimal Launch Date for Interplanetary Missions
Hypersonic Point-to-Point Travel for the Common Man
Evolutionary Optimisation of a Flexible-Launcher Simple Adaptive Control System
Near-Optimal Guidance and Pulse-Modulated Reduced-Attitude Control for Orbit Injection
Optimized Packings in Space Engineering Applications: Part II
A Pareto Front Numerical Reconstruction Strategy Applied to a Satellite System Conceptual Design