首页> 外文会议>SAE Aerospace Systems and Technology Conference >Airship Positioning Fuzzy Multi-Ballonet Control Study
【24h】

Airship Positioning Fuzzy Multi-Ballonet Control Study

机译:飞艇定位模糊多气球控制研究

获取原文

摘要

Airship designers research application versions of systems with several ballonets for adjustment of airship roll and/or pitch as a whole. This requires effective automatic status management of each separate ballonet. But multi-ballonet system control issue encounters the absence of industrially measurable variables of each separate ballonet status. Thus status control issue of the system becomes uncertain. The fact requires the issue studying and shaping new scientific and technical solutions. This publication represents research results implying that fairly simple implementation and effective result can be achieved by application of fuzzy control concept. Its application is built on generating the representative quantity of fuzzy production rules. They are based on present set evaluation of known parameters and measured variables. This results in fuzzy but meaningful image of ballonet system status and airship as a whole. Thus achieving fairly good control over multi-ballonet system. This article represents development results of fuzzy automatic control system version of two-ballonet system containing determined positional control systems of pressure difference between body gas environment and atmosphere. The resulted hybrid control system maintains necessary pressure in airship body and provides airship trim control efficiency at low traveling speed. Modes like that appear during take-off and landing. The development is based upon airship model with ballonet control system which adequacy has been checked by previous researches. This model was used to research and experimentally correct conditions and influence results of developed production rules on ballonet system status and airship as a whole. Control law fuzzy derivation procedure is demonstrated and explained. Described is simulation modeling diagram of fuzzy control hybrid system of two-ballonet system in Simulink environment and its computer testing results. Illustrated is airship positioning fuzzy control maintaining boost pressure in body to provide its specified rigidity.
机译:飞艇设计师研究应用程序版本,具有几个气球,用于调整飞艇卷和/或整体俯仰。这需要每个单独的气球的有效自动状态管理。但是,多气球系统控制问题遇到了每个单独的气球状态的工业上可测量变量的缺失。因此,系统的状态控制问题变得不确定。事实要求问题研究和塑造新的科技解决方案。本出版物代表了研究结果,这意味着通过应用模糊控制概念,可以实现相当简单的实施和有效的结果。它的应用是为生成模糊生产规则的代表性数量而建立的。它们基于本发明的已知参数和测量变量的设置评估。这导致模糊但是整个气球系统状态和飞艇的图像。从而实现了对多气球系统的相当良好的控制。本文代表了在体内气体环境与大气之间的压力差异的确定位置控制系统的双气球系统模糊自动控制系统版的开发结果。由此产生的混合控制系统在飞艇机构中保持必要的压力,并以低行进速度提供飞艇调节控制效率。像起飞和着陆期间出现的模式。该开发基于Ballonet控制系统的飞艇模型,通过以前的研究已经过了充分的研究。该型号用于研究和实验纠正和实际纠正现状的条件,以及整个运动系统现状和飞艇开发的生产规则的结果。对照法展示和解释了控制法模糊推导程序。描述了Simulink环境中双气球系统模糊控制混合系统仿真建模图及其计算机测试结果。所示是飞艇定位模糊控制,维持身体的增压,以提供其特定刚性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号