A multi-model and multi-objective approach to the design of helicopter flight control laws

Author:

Authié Patrick

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference16 articles.

1. Stiles, L.R., Mayo, J., Freisner, A.L., Landis, K.H., and Kothmann, B.D.: Impossible to Resist: The Development of Rotorcraft Fly-by-Wire Technology. In American Helicopter Society $$60^{th}$$ Annual Forum (2004)

2. Huo, J., Gu, H.: Survey on flight control technology for large-scale helicopter. Int. J. Aerosp. Eng. 2017(02), 1–14 (2017)

3. Anonymous.: Aeronautical Design Standard - Performance Specification. Handling Qualities Requirements for Military Rotorcraft ADS-33E-PRF, March (2000)

4. Tischler, M., Colbourne, J., Morel, M., Biezad, D., Levine, W., Moldoveanu, V.: CONDUIT: a new multidisciplinary integration environment for flight control development (1997)

5. Antonioli, J.C., Taghizad, A., Rakotomamonjy, T., Ouladsine, M.: Helicopter flight control design tool integrating handling qualities. In $$5^{th}$$ European Conference for Aerospace Sciences (EUCASS) (2013)

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