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
收藏
页码：81 / 86
页数：6
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