Two‐stage construction of aircraft thrust models for optimal control computations | Zendy

Miller Janusz | Zendy; Korytowski Adam | Zendy; Szymkat Maciej | Zendy

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Two‐stage construction of aircraft thrust models for optimal control computations

Author(s) -

Miller Janusz,

Korytowski Adam,

Szymkat Maciej

Publication year - 2008

Publication title -

optimal control applications and methods

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.458

H-Index - 44

eISSN - 1099-1514

pISSN - 0143-2087

DOI - 10.1002/oca.835

Subject(s) - computation , thrust , stage (stratigraphy) , optimal control , mathematical optimization , control theory (sociology) , control (management) , computer science , aerospace engineering , engineering , mathematics , geology , algorithm , artificial intelligence , paleontology

A two‐stage method for building analytic models based on experimental data is proposed. It is applied to thrust modeling for the F‐15 aircraft. A minimum‐time problem is solved to show efficacy of the models in indirect optimal control computations. Copyright © 2008 John Wiley & Sons, Ltd.

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