Robust Design Method for Flight Control System of Cruise Missile
The flight control system design method of wing-in-ground effect aircraft is presented based on robust control theory. With a view to uncertainty of lengthways channels, the simplified mathematical model is constituted for wing-in-ground effect aircraft. According to this simplified model, the lengthways control system is designed. In order to overcome defect of uncertain system, the flight controller of wing-in-ground effect aircraft is designed using robust control theory. Simulation results show that this control method can implement efficiently precision control mission for wing-in-ground effect aircraft as well as preferable robustness.
Yongxin Yin Zhongming Ou Wen Shi
Engineer at China Academy of Aerospace Aerodynamics,Beijing,China.Research interests include guidanc Researcher at China Academy of Aerospace Aerodynamics,Beijing,China.Research interests include fligh Researcher at China Academy of Aerospace Aerodynamics,Beijing,China.Research interests include fligh
国际会议
哈尔滨
英文
1452-1454
2010-01-08（万方平台首次上网日期，不代表论文的发表时间）