Discrete Variable Structure Control Design for APCS of Carrier-based Aircraft Based on Dynamic Disturbance Compensation
Based on introduction and analysis of approach power compensation system (APCS) of carrierbased aircraft, the design problem of approach power compensation system via discrete variable structure control theory is researched and figured out with the use of discrete variable structure control theory bases on disturbance compensation. Furthermore, the chattering phenomenon of the proposed variable structure control system is weakened by using hyperbolic tangent function instead of conventional sign function. Simulation results indicate that the new system owns well performance in path tracking and reducing the influence of airflow disturbance.
Qi-dan ZHU Yong-tao YU Wen ZHANG
Department of Automation, Harbin Engineering University, Harbin, China
国际会议
长春
英文
1671-1675
2011-09-03(万方平台首次上网日期,不代表论文的发表时间)