Receding horizon control of an F-16 aircraft: A comparative study

被引：49

作者：

Keviczky, Tamas ^{[1
]}

Balas, Gary J. ^{[1
]}

机构：

[1] Univ Minnesota, Dept Aerosp Engn & Mech, Minneapolis, MN 55455 USA

来源：

CONTROL ENGINEERING PRACTICE | 2006年 / 14卷 / 09期

关键词：

predictive control; flight control; optimization;

D O I：

10.1016/j.conengprac.2005.06.003

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 comparison between receding horizon control (RHC) approaches is presented for the longitudinal axis control of an F-16 aircraft. The results suggest that the flexibility provided by a scheduled RHC scheme based on flight condition-dependent linear prediction models is a necessary requirement for achieving good performance as opposed to a single LTI model-based method. The scheduled scheme offers an attractive alternative to a full nonlinear model-based RHC approach by trading off an acceptable degradation in performance to modest computational complexity and real-time implementability. (c) 2005 Elsevier Ltd. All rights reserved.

引用

页码：1023 / 1033

页数：11

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