This article presents the motivation, goals and benchmark problems of a study from the European Space Agency entitled "Robust Flight Control System Design Verification and Validation Framework" (RFCS). The objective of the study is to develop, demonstrate and compare the potential of modern control design, analysis and modeling techniques to address complex issues currently not well covered in the traditional launchers' verification and validation (V&V) process. The identification of these V&V gaps have resulted in a set of benchmark problems that allow comparing the standard results with those arising from the application of the advanced techniques. The benchmark problems are extracted from the VEGA launcher and its V&V process, but their significance is more general as they represent common issues found in most launchers.
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