Title of article
Optimal input design for aircraft parameter estimation
Author/Authors
Jauberthie، نويسنده , , Carine and Bournonville، نويسنده , , François and Coton، نويسنده , , Patricia and Rendell، نويسنده , , Frank، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2006
Pages
7
From page
331
To page
337
Abstract
An optimal input design technique for aircraft parameter estimation is presented in this paper. The original idea is the combination of a dynamic programming method with a gradient algorithm for the optimal input synthesis. This approach allows to include realistic practical constraints on the input and output variables. A description of this approach is presented, followed by an example concerning an aircraft longitudinal flight.
Keywords
Nonlinear controlled systems , Optimal input design , Parameter estimation , Systèmes non linéaires contrôlés , Planification dיentrée optimale , Estimation de paramètres
Journal title
Aerospace Science and Technology
Serial Year
2006
Journal title
Aerospace Science and Technology
Record number
2229500
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