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  • 标题:Robust Multivariable controller Design with the simultaneous H2 /H∞/µ for Single Person Aircraft
  • 其他标题:Robust Multivariable controller Design with the simultaneous H2 /H∞/µ for Single Person Aircraft
  • 作者:Javad Mashayekhi Fard ; Mohammad Ali Nekoui ; Ali Khaki Sedigh
  • 期刊名称:International Journal of Electrical and Computer Engineering
  • 电子版ISSN:2088-8708
  • 出版年度:2013
  • 卷号:3
  • 期号:2
  • 页码:279-286
  • 语种:English
  • 出版社:Institute of Advanced Engineering and Science (IAES)
  • 摘要:In a physical system several targets are normally being considered in which each of nominal and robust performance has their own strengths and weaknesses. In nominal performance case, system operation without uncertainty has decisive effect on the operation of system, whereas in robust performance one, operation with uncertainty will be considered. The target of present paper is a balance between nominal and robust performance of state feedback A new approach of present paper is the combination of two controllers of μ and H2/H∞. The controller for robust stability status, nominal performance, robust performance and noise rejection are designed simultaneous. Controller will be achieved from solving constraint optimization problem. Where a simultaneous H2 /H∞/µ robust multivariable controller has been designed over an X-29 Single Person. This model has three inputs and three outputs, where the state space equations of the system response to an unstable one. Simulation results show the effectiveness and benefits of the method.DOI:http://dx.doi.org/10.11591/ijece.v3i2.2352
  • 其他摘要:In a physical system several targets are normally being considered in which each of nominal and robust performance has their own strengths and weaknesses. In nominal performance case, system operation without uncertainty has decisive effect on the operation of system, whereas in robust performance one, operation with uncertainty will be considered. The target of present paper is a balance between nominal and robust performance of state feedback A new approach of present paper is the combination of two controllers of μ and H 2 /H ∞ . The controller for robust stability status, nominal performance, robust performance and noise rejection are designed simultaneous. Controller will be achieved from solving constraint optimization problem. Where a simultaneous H 2 /H ∞ /µ robust multivariable controller has been designed over an X-29 Single Person. This model has three inputs and three outputs, where the state space equations of the system response to an unstable one. Simulation results show the effectiveness and benefits of the method. DOI: http://dx.doi.org/10.11591/ijece.v3i2.2352
  • 关键词:H2 /H∞/µ Robust Controller - Multi-Objective Control - Constraint optimization - Single Person Aircraft
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