Optimal input design for a nonlinear dynamical uncertain aerospace system
نویسندگان
چکیده
منابع مشابه
Optimal Input Design for a Nonlinear Dynamical Uncertain Aerospace System
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...
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ژورنال
عنوان ژورنال: IFAC Proceedings Volumes
سال: 2013
ISSN: 1474-6670
DOI: 10.3182/20130904-3-fr-2041.00060