The Control Allocation of Flying Saucer with Uncertainties
In order to harmonize the actions between thrust vectoring control and mass control of the flying saucer, the control allocation was used to design the input control commands. The variable structure control was used to generate the virtual control law. The actuator dynamics was considered. In order to improve the robustness of the system, the uncertainties of the aerodynamic coefficients of the system were also considered in control allocation. Simulation results show that the proposed method is right and effective.
control of aerocraft robustness control allocation variable structure control
Wu Yinsheng Leng Huazhi Zhang Youan
Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai, Shandong Naval Command College, Nanjing, Jiangsu 211800, China
国际会议
2009年中国控制与决策会议(2009 Chinese Control and Decision Conference)
广西桂林
英文
3402-3405
2009-06-17（万方平台首次上网日期，不代表论文的发表时间）