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Article Dans Une Revue Aerospace Science and Technology Année : 2006

Optimal input design for aircraft parameter estimation

Résumé

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.

Dates et versions

hal-01740533 , version 1 (22-03-2018)

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Carine Jauberthie, François Bournonville, Patricia Coton, Frank Rendell. Optimal input design for aircraft parameter estimation. Aerospace Science and Technology, 2006, 10 (4), pp.331 - 337. ⟨10.1016/j.ast.2005.08.002⟩. ⟨hal-01740533⟩
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