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�������պ����ѧѧ�� 2010, Vol. 36 Issue (11) :1353-1357    DOI:
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��Ϊ, ���ܸ�, ����, �����*
�������պ����ѧ ��ͨ��ѧ�빤��ѧԺ, ���� 100191
Vehicular DYC via SMC and system stability analysis
Zhang Wei, Ding Nenggen, Wang Jian, Yu Guizhen*
School of Transportation Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

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ժҪ ֱ�Ӻ�����ؿ���(DYC,Direct Yaw Moment Control)���ڼ��޹����²���ά�ֳ����ȶ���ʻ����ĸ��Ӻ������,�Ӷ����������������ȫ����.�������ܹ����������ȶ��Կ��Ʋ���Ҫ��ķ�������������ѧģ��,�������������DYC�Ļ�ģ��ṹ������(SMC,Sliding Mode Controller),���������Ϻ���֤����ϵͳ���ȶ���,�����Matlab/Simulink�����¶�SMC���ȶ��ԺͿ���Ч�������˷������.�����������˿����㷨����Ч��,��ͨ����PID(Proportional-Integral-Derivative)�㷨����Ч���ĶԱ�˵����SMC���и��õ�³����,ӵ�и��õ�Ӧ��DZ��.
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Abstract�� Direct yaw moment control (DYC) can generate the additional yaw-moment needed to maintain vehicle stability in the limit conditions so to improve the active safety of a vehicle-s handling. A nonlinear vehicle dynamic model which meets the requirements of vehicle stability control experiments was established, and a sliding mode controller (SMC) was designed. The stability of the SMC controller was proved with Lyapunov function. At last the stability and control effect of the SMC was verified by simulations in Matlab/Simulink. The simulation results prove the effectiveness of the control algorithm and suggeste that the robustness of SMC is better than that of proportional-integral-derivative(PID) control algorithm, which proves SMC better application potential.
Keywords�� direct yaw moment control   sliding mode controller   stability analysis     
Received 2009-06-16;

������Ȼ��ѧ����������Ŀ(50908008); ����"863"�ƻ�������Ŀ (2009AA11Z216)

Corresponding Authors: ��Ϊ     Email: zhw@ae.buaa.edu.cn
About author: �� Ϊ(1981-),��,������ԭ��,��ʿ��,zhw@ae.buaa.edu.cn.
��Ϊ, ���ܸ�, ����, �����.����DYC��ģ��������Ƽ�ϵͳ�ȶ��Է���[J]  �������պ����ѧѧ��, 2010,V36(11): 1353-1357
Zhang Wei, Ding Nenggen, Wang Jian, Yu Guizhen.Vehicular DYC via SMC and system stability analysis[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2010,V36(11): 1353-1357
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