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Optimal input design for aircraft parameter estimation

delete2006-05-01
delete14
PRE
AI
C
Carine Jauberthie *
F
François Bournonville
P
Patricia Coton
F
Frank Rendell
DOI：10.1016/j.ast.2005.08.002delete
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Abstract

Abstract

En 中文
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. (c) 2005 Elsevier SAS. All rights reserved.
Keywords:
nonlinear controlled systems
optimal input design
parameter estimation
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Key information extracted from the uploaded paper, including a brief overview, abstract, background, key highlights, visual analysis, and future outlook.

Journal

Aerospace Science and Technology cover
Aerospace Science and Technology
IF:
5.8
Papers:
1.0W
Citations:
3.0W

Organization

No organization information available