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Optimal input design for a nonlinear dynamical uncertain aerospace system

Carine Jauberthie 1 Elodie Chanthery 1
1 LAAS-DISCO - Équipe DIagnostic, Supervision et COnduite
LAAS - Laboratoire d'analyse et d'architecture des systèmes
Abstract : An optimal input design technique for aircraft uncertain parameter estimation is presented in this paper. The original idea is the combining of a dynamic programming method and interval analysis for the optimal input synthesis. This approach does not imply the estimation of a nominal value for parameter and allows to include realistic practical constraints on the input and output variables. The precise description of the approach is followed by an application in aerospace sciences.
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Contributor : Carine Jauberthie <>
Submitted on : Friday, December 28, 2018 - 10:56:35 AM
Last modification on : Thursday, June 10, 2021 - 3:01:27 AM
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  • HAL Id : hal-01966336, version 1


Carine Jauberthie, Elodie Chanthery. Optimal input design for a nonlinear dynamical uncertain aerospace system. IFAC Symposium on Nonlinear Control Systems, Sep 2013, Toulouse, France. ⟨hal-01966336⟩



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