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�������պ����ѧѧ�� 2002, Vol. 28 Issue (3) :257-260    DOI:
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Reconfiguration of Control Surface Faults with Thrust Vectoring Technique
ZHANG Ping, CHEN Zong-ji*
Beijing University of Aeronautics and Astronautics, School of Automation Science and Electrical Engineering

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Abstract�� The compensating effect of thrust vectoring technique on aerodynamics of an aircraft in its pitch and yaw motions was discussed. Attention was focused on how to realize reconfiguration of the control law with thrust vectoring technique when any failure of the control surface appears in flight.Definition of control redundancy and sufficient conditions of Pseudo inverse reconfiguration were given. An example of rudder fault of the aircraft was illustrated, satisfactory reconfiguration results were obtained with the above technique.
Keywords�� fault-tolerant technique   reconstitution   flight control   self-repairing systems   thrust vectoring control     
Received 2000-07-11;
Fund:

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��ƽ, ���ڻ�.����ʸ���Էɻ�������ʧЧ�IJ������ع�[J]  �������պ����ѧѧ��, 2002,V28(3): 257-260
ZHANG Ping, CHEN Zong-ji.Reconfiguration of Control Surface Faults with Thrust Vectoring Technique[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2002,V28(3): 257-260
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http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2002/V28/I3/257
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