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The cost associated with developing flight control forms a significant partof the overall development cost. The increased demand for greater functionalityand for extending the domain of applicability of future launchers leads tohigher complexity of the GNC algorithms. Furthermore, there is also a need fora responsive design methodology, which can quickly adapt to changes in therequirements during the development process. These demands are stretching thecurrent,largely manual, development process, which is fragmented in thedifferent disciplines and activities concerning modelling, algorithm design,software coding, implementation on the avionics platform and the associatedtesting at the different stages. The model-based-design (MBD) philosophypresents an attractive solution in addressing the multi-disciplinary nature ofthe flight algorithm design task. In terms of design process, this materializesin a tight coupling between the modelling, the design and the analysisactivities.An integrated design framework for the GNC development for futurelauncher upper stages has been realized.

Model Based Desgin Environment for Launcher Upper Stage GNC Development