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Aircraft Dynamics Identification for Optimal Control

Abstract : Four new Maximum Likelihood based approaches for aircraft dynamics identification are presented and compared. The motivation is the need of accurate dynamic models for minimizing aircraft fuel consumption using optimal control techniques. A robust method for building aerodynamic models is also suggested. All these approaches were validated using real flight data from 25 different aircraft.
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Contributor : Cédric Rommel Connect in order to contact the contributor
Submitted on : Monday, November 20, 2017 - 3:28:13 PM
Last modification on : Thursday, January 20, 2022 - 5:31:29 PM
Long-term archiving on: : Wednesday, February 21, 2018 - 2:48:43 PM


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Cédric Rommel, Joseph Frédéric Bonnans, Baptiste Gregorutti, Pierre Martinon. Aircraft Dynamics Identification for Optimal Control. 7th European Conference on Aeronautics and Space Sciences (EUCASS 2017), Jul 2017, Milan, Italy. ⟨10.13009/EUCASS2017-179⟩. ⟨hal-01639731⟩



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