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

被引：0
|
作者：
Miller, Janusz [1 ]
Korytowski, Adam [1 ]
Szymkat, Maciej [1 ]
机构：
[1] AGH Univ Sci & Technol, Inst Automat Control, PL-30059 Krakow, Poland
来源：
OPTIMAL CONTROL APPLICATIONS & METHODS | 2008年 / 29卷 / 05期
关键词：
thrust modeling; optimal control; numerical approximation; sensitivity;
D O I：
10.1002/oca.835
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
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 (C) 2008 John Wiley & Sons, Ltd.
引用
收藏
页码：393 / 406
页数：14
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