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�������պ����ѧѧ�� 1998, Vol. 24 Issue (3) :283-286    DOI:
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Design of Integrated Flight/Vectored Nozzle Control System at Take-Off
Peng Kemao, Shen Gongzhang, Wen Chuanyuan*
Beijing University of Aeronautics and Astronautics,Dept of Automatic Control

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Abstract�� Four kind of configurations are adopted to analyze the improvement of the vectored nozzle control on the flight performances at take-off,where the baseline aircraft is modified to add the horizontal canard or/and vectored nozzle�� The models of the aircraft longitudinal motion at the different progresses of the take-off are established�� The system controllers of the integrated flight/vectored nozzle control system at take-off are respectively designed according to the configurations�� The simulations of the aircraft at take-off are made on the established models and nonlinear propulsion system model�� The results prove that the designed system controllers are available to implement the take-off mission�� The major specifications prove that the vectored nozzle control can significantly improve the flight performances at take-off when appropriately coordinated with the aerodynamic control effectors
Keywords�� flight control systems   thrust vector control   performance analysis     
Received 1997-01-23;


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���ï, �깦�, �Ĵ�Դ.���ģ̬���ۺϷ���ʸ����ܿ���ϵͳ���[J]  �������պ����ѧѧ��, 1998,V24(3): 283-286
Peng Kemao, Shen Gongzhang, Wen Chuanyuan.Design of Integrated Flight/Vectored Nozzle Control System at Take-Off[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 1998,V24(3): 283-286
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