| 小型验证飞艇气体压力控制系统设计 |
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| 引用本文： | 曹毅,罗传勇,罗义平,王宏力.小型验证飞艇气体压力控制系统设计[J].电光与控制,2007,14(4):180-182,186. |
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| 作者姓名： | 曹毅 罗传勇 罗义平 王宏力 |
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| 作者单位： | 1. 第二炮兵工程学院,西安,710025
2. 湖南航天局浮空器研发中心,长沙,410205 |
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| 摘 要： | 介绍了小型验证飞艇中压力控制系统的主要设计方案,尤其是控制系统的核心--控制器的设计方法.针对囊体内的压力控制具有明显的非线性和模型不确定性的特点,在数字PID控制的基础上提出了将智能控制理论应用到飞艇压力控制系统设计中的设计方法,以达到更精确有效的控制.
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| 关 键 词： | 软式飞艇 压力控制 PID控制 智能控制 |
| 文章编号： | 1671-637X（2007）04-0180-03 |
| 修稿时间： | 2006-02-142006-03-10 |
Design of gas pressure control system for small verifying airship |
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| CAO Yi,LUO Chuan-yong,LUO Yi-ping,WANG Hong-li.Design of gas pressure control system for small verifying airship[J].Electronics Optics & Control,2007,14(4):180-182,186. |
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| Authors: | CAO Yi LUO Chuan-yong LUO Yi-ping WANG Hong-li |
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| Abstract: | The design scheme of the gas pressure control system of small verifying airship, especially the design method of controller, which is the core of the control system, is discussed in this paper. Since the control of gas pressure in the cell has obvious nonlinearity and the model is uncertainty, the intelligent control theory is applied on the basis of digital PID control theory to achieve more precise control effect. |
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| Keywords: | non-rigid Airship pressure control digital PID control intelligent control |
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