Volume 22 Issue 1
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WANG Yong-ting, GUO Ying-qing, WANG Hai-guan. Augmented LQL method and its application to aeroengine control[J]. Journal of Aerospace Power, 2007, 22(1): 132-136.
Citation: WANG Yong-ting, GUO Ying-qing, WANG Hai-guan. Augmented LQL method and its application to aeroengine control[J]. Journal of Aerospace Power, 2007, 22(1): 132-136.
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Augmented LQL method and its application to aeroengine control

  • School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China

  • Received Date: 2005-10-26
  • Rev Recd Date: 2006-02-26
  • Publish Date: 2007-01-28
    Abstract
  • LQL（Linear quadratic L2 bounded uncertainties）control method was applied to the aeroengine control system.The augmented LQL method was proposed,then the aeroengine control system was designed by using the method.Simulation of the control system in the flight envelope was performed,and excellent tracking performance and robustness were obtained.

     

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    • References(4)
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    陈善本,范颖晖.具L2有界不确定性系统线性二次鲁棒最优控制--LQL方法[M].北京:科学出版社,2004.
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    杨刚,孙健国,李秋红.航空发动机控制系统中的增广LQR方法[J].航空动力学报,2004,19(1):153-158.YANG Gang,SUN Jianguo,LI Qiuhong.Augmented LQR method for aeroengine control systems[J].Journal of Aerospace Power,2004,19(1):153-158.
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