Abstract
Within the joint project AeroStruct, the Department of Flight Mechanics, Flight Control and Aeroelasticity at TU Berlin developed generic flight control modules for considering the influence of flight control functions in preliminary aircraft design. In order to improve the methods used for the design process, an automated tool chain was set up, that builts a flight-mechanical model of the airplane, calculates controller parameters according to consistent criteria and automatically implements flight control functions in a high fidelity simulation environment.
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References
Flying Qualities of Piloted Aircraft, MIL-HDBK-1797A, US Navy (1997)
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Hamann, A. (2018). Development of Flight Control Functions for Integration in Gust Load Simulations. In: Heinrich, R. (eds) AeroStruct: Enable and Learn How to Integrate Flexibility in Design. AeroStruct 2015. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 138. Springer, Cham. https://doi.org/10.1007/978-3-319-72020-3_4
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DOI: https://doi.org/10.1007/978-3-319-72020-3_4
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Publisher Name: Springer, Cham
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Online ISBN: 978-3-319-72020-3
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