Multi-objective Optimal Longitudinal Flight Control System Design for Large Flexible Transport Aircraft

被引：0

作者：

Song, Sipeng ^{[1
]}

Whidborne, James F. ^{[1
]}

Lone, Mudassir ^{[1
]}

Molina-Cristobal, Arturo ^{[1
]}

机构：

[1] Cranfield Univ, Ctr Aeronaut, Cranfield, Beds, England

来源：

2018 UKACC 12TH INTERNATIONAL CONFERENCE ON CONTROL (CONTROL) | 2018年

关键词：

ROBUST-CONTROL; OPTIMIZATION; PERFORMANCE; LIMITS;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper presents a multi-objective evolutionary algorithm design of a longitudinal optimal controller for a large flexible transport aircraft. The algorithm uses a mixed optimization approach based on a combination of Linear Quadratic Regulator (LQR) control and a Multi-Objective Genetic Algorithm (MOGA) to search over a set of possible weighting function structures and parameter values in order to satisfy a number of conflicting design criteria. The proposed approach offers a number of potential optimal solutions lying on or near the Pareto optimal front of competing objectives. The approach is explained in this paper and some results are presented.

引用

页码：81 / 86

页数：6

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