Furthermore, requirements for the processes and methods will be derived and parameter uncertainties will be considered. For this purpose, interfaces between the involved disciplines will be defined and implemented. The assessment will be provided up to the aircraft level to evaluate the flight control systems regarding global parameters like estimation of loads, power consumption and mass. Therefore, the focus of the group lies in the development of rapid preliminary design processes for aircraft including an early consideration of system aspects. The group develops rapid preliminary design process This leads to the fact that the design of new and unconventional configurations, characterised by reduced emissions and costs, is going to be much more difficult and expensive.
Consequently, for finding global optimums additional degrees of freedom cannot be used in the optimisation stage. System aspects are considered late in the design process and must meet the given requirements of the prior disciplines. The design of flight control systems is a multidisciplinary optimisation process which is driven by aerodynamic aspects. To accomplish these objectives, the research focuses on the following core areas.įocus: Rapid Preliminary Design Processes The objective of the team “Safety-Critical Architectures” is the development of concepts and assessment methods for modern architectures with maximum robustness and flexibility regarding reconfigurations. The reliability of these systems is crucial for humans as well as for the aircraft itself.
Flight control systems are an important part of the safety-critical system architectures of an aeroplane.
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