This involves the system-level implementation of innovative functions, such as active load alleviation and flutter suppression, through multifunctional control surfaces utilizing representative system components. The systems of the demonstrator are being designed from scratch, taking into account the usual certification requirements in aviation, including CS-25, etc. The design was, furthermore, tailored to future commercial transport aircraft.
The demonstrator includes flight control systems for multifunctional control surfaces as well as a load simulation system. A flight dynamics model including load simulation is being executed on a powerful simulation computer to provide the necessary commands in real-time for the flight control systems and the load simulation system.
Beyond the end of the project, the demonstrator will remain available for further development of multifunctional flight control systems.
Institutes involved
- DLR Institute of Flight Systems
- DLR Institute of Aeroelasticity
- DLR Institute of System Dynamics and Control
- DLR Institute of Lightweight Systems
Partners involved
Liebherr-Aerospace Lindenberg GmbH, Diehl Aerospace GmbH, FFT Produktionssysteme GmbH, Technische Universität Berlin
Funding organisations
BMWK, LuFo VI-2