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纵向着舰二阶自抗扰导引控制律设计
引用本文:李冀鑫,侯志强,郑小洪,贾忠湖.纵向着舰二阶自抗扰导引控制律设计[J].海军航空工程学院学报,2008,23(2):139-142.
作者姓名:李冀鑫  侯志强  郑小洪  贾忠湖
作者单位:1. 海军航空工程学院研究生管理大队,山东,烟台,264001
2. 海军航空工程学院飞行器工程系,山东,烟台,264001
摘    要:在阐述自动着舰系统和自抗扰控制器工作原理的基础上,设计了纵向着舰导引自抗扰控制器。仿真结果表明,自抗扰导引控制器对典型输入的跟踪性能良好,抑制突风扰动的能力较强,闭环系统响应的快速性和超调量均优于经典PID控制效果。

关 键 词:舰载飞机  自抗扰控制  自动着舰  导引
文章编号:1673-1522(2008)02-0139-04
修稿时间:2007年10月15

Design of Longitudinal Carrier Landing Guidance Law Based on ADRC
LI Ji-xin,HOU Zhi-qiang,ZHENG Xiao-honga and JIA Zhong-hub.Design of Longitudinal Carrier Landing Guidance Law Based on ADRC[J].Journal of Naval Aeronautical Engineering Institute,2008,23(2):139-142.
Authors:LI Ji-xin  HOU Zhi-qiang  ZHENG Xiao-honga and JIA Zhong-hub
Institution:QU Jun-wu, ZHAO Guo-rong, KOU Kun-hu (Naval Aeronautical and Astronautical University a. Graduate Students' Brigade; b. Department of Control Engineering, Yantai Shandong 264001, China)
Abstract:There are many strongpoints in the Longitudinal Block Diagonal Control system because it adopts parsing dissolution. However controller has problems of more parameters and difficult optimizing choice by experience. In this paper, a project was proposed that controller parameters were optimized by particle swarm optimization (PSO), and it was being principle analysis and simulation of numerical value. The results demonstrate this project can automatic optimize controller parameters, and it achieves precision path tracking when carrier landing of the carrier aircraft.
Keywords:carrier-base airplane  ADRC  automatic carrier landing  guidance
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