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�������պ����ѧѧ�� 2011, Vol. 37 Issue (10) :1312-1316    DOI: CNKI:11-2625/V.20111020.1126.009
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Subsystem disturbance rejection control of turbo-shaft engine/helicopter based on cascade ADRC
Sun Liguo, Wang Rixian, Sun Jianguo, Zhang Haibo*
College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

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ժҪ ��Ҫ�о����ᷢ����ת�ٿ��ſ�������,�����һ�ֻ����Կ��ſ��Ƽ���(ADRC, Adaptive Disturbance Rejection Control)�����ᷢ���������ʹ������ſ�������Ʒ���.һ����,���ô������ƽṹ,�ڻ����ƿ�ģ̬��ȼ������ת��,�⻷���ƹ�������ת��,ʹ���ڻ��Ŷ��õ���������.��һ����,ÿ���ӻ�·��ͨ������״̬���۲�ʵʱ�ضԱ��ض����ڻ������Ŷ�����.���,����ֱ����/�������������ۺϷ���ģ�͵����ַ�������ÿ��Ʒ����������������ᷢ�������ʸ�������,������ֱ����/���ᷢ�����ۺϱջ�ϵͳ�Ŀɲٿؼ���.
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Abstract�� Disturbance rejection control problem of turbo-shaft engine speed was studied. A disturbance rejection control scheme of turbo-shaft engine was proposed based on increment cascade adaptive disturbance rejection control (ICADRC). For one thing, cascade control structure was used to ensure that the disturbance in the inner loop can be suppressed in time. In this control structure, gas turbine speed was controlled in the inner loop, while power turbine speed in the outer loop. For another, in both control loops the control object was compensated from disturbance in virtue of extended state observation. Finally, digital simulation of integrated helicopter/engine system shows that the new control scheme can improve the power following character of turbo-shaft engine evidently, and can enhance the handling limit of integrated helicopter/engine closed loop system.
Keywords�� engine/helicopter   cascade ADRC   speed control   subsystem   compensation from disturbance     
Received 2010-05-30;


About author: ������(1984-),��,�ӱ�������,˶ʿ��,sunliguo@nuaa.edu.cn.
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Sun Liguo, Wang Rixian, Sun Jianguo, Zhang Haibo.Subsystem disturbance rejection control of turbo-shaft engine/helicopter based on cascade ADRC[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2011,V37(10): 1312-1316
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