基于PID控制的垂直发射控制技术
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(1.海军航空工程学院 控制工程系,山东 烟台 264001;2.江西师范大学 物理与通信电子学院,南昌 330000)

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TJ765.2+3

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Vertically Launched Technology Based on PID Control
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(1.Department of Control Engineering,NAAU,Yantai Shandong 264001,China;2.College of Physics and Communication Electronics of Jiangxi Normal University,Nanchang 330000,China)

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    摘要:

    基于对PID控制的垂直发射控制技术的研究,针对导弹的垂直发射问题,文章阐述了:① 建立了气动舵/推力矢量复合控制的模型;② 提出了一种能够实现垂直发射快速转弯的程序弹道指令设计方法,并设计了导弹3个通道的PID控制器;③ 通过对弹道进行6DOF仿真分析,验证了指令和控制器设计的正确性和有效性。

    Abstract:

    Based on the study of vertically launched technology using PID control, in this paper, the problems of vertical launch were solved. First, the model of integrated aerofin/thrust vector control missile was built. Second, a kind of arc trajectory design method which could achieve the quick turning of vertically launched missiles was introduced, and PID controller of three channels was designed respectively. Finally, a 6-degree trajectory simulation analysis of missile was made to validate the correctness and effectiveness of trajectory design and controller design theory.

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引用本文

黄剑华,耿宝亮,胡云安.基于PID控制的垂直发射控制技术[J].海军航空大学学报,2008,23(5):513-516, 520
HUANG Jian-hua, GENG Bao-liang, HU Yun-an. Vertically Launched Technology Based on PID Control[J]. JOURNAL OF NAVAL AVIATION UNIVERSITY,2008,23(5):513-516, 520

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  • 在线发布日期: 2018-07-05
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