Aircraft Landing Gear Control with Multi-Objective Optimization Using Generalized Cell Mapping

被引：0

作者：

孙建桥 ^{[1
,2
]}

贾腾 ^{[1
]}

熊夫睿 ^{[1
]}

秦志昌 ^{[1
]}

吴卫国 ^{[1
]}

丁千 ^{[1
]}

机构：

[1] School of Mechanical Engineering, Tianjin University

[2] School of Engineering, University of

来源：

Transactions of Tianjin University | 2015年 / 02期

关键词：

D O I：

暂无

中图分类号：

O221.6 [多目标规划];

学科分类号：

摘要：

This paper presents a numerical algorithm tuning aircraft landing gear control system with three objectives,including reducing relative vibration, reducing hydraulic strut force and controlling energy consumption. Sliding mode control is applied to the vibration control of a simplified landing gear model with uncertainty. A two-stage generalized cell mapping algorithm is applied to search the Pareto set with gradient-free scheme. Drop test simulations over uneven runway show that the vibration and force interaction can be considerably reduced, and the Pareto optimum form a tight range in time domain.

引用

页码：140 / 146

页数：7

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