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Development of Flight Control Functions for Integration in Gust Load Simulations

  • Alexander HamannEmail author
Conference paper
Part of the Notes on Numerical Fluid Mechanics and Multidisciplinary Design book series (NNFM, volume 138)

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.

References

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    Flying Qualities of Piloted Aircraft, MIL-HDBK-1797A, US Navy (1997)Google Scholar
  2. 2.
    Military Specification: Flying Qualities of Piloted Airplanes MIL-F-8785C, US Navy (1980)Google Scholar

Copyright information

© Springer International Publishing AG 2018

Authors and Affiliations

  1. 1.Department of Flight MechanicsFlight Control and AeroelasticityBerlinGermany

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