Control Law Design of Aircraft Super-maneuverable Flight Based on Dynamic Surface Backstepping Control
It proposed a dynamic surface backstepping control for super-maneuverable flight. In contrast to the basic backstepping method, our scheme abandons the adaptive laws, and introduces sliding surfaces and reaching conditions to design the virtual control signal and the final control signal. Furthermore, instead of involving model differentiation, a low pass dynamic filter is used in the two steps backstepping design, which provides a more simplified control algorithm. The simulation results show that the new scheme achieves a simple design procedure and a satisfying tracking performance.
Adaptive Control Super-maneuver Flight Flight Control Dynamic Surface Control Backstepping
LIU Shu-guang SUN Xiu-xia DONG Wen-han SONG Hong-fei
Engineering Institute, Air Force Engineering University, Xi’an 710038
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
1764-1768
2009-06-17（万方平台首次上网日期，不代表论文的发表时间）