Title :
Fuzzy Sliding mode Control for missile autopilot design
Author :
Sadr, Negar Elmi ; Momeni, Hamid Reza
Author_Institution :
Fac. of Electr. Eng., Tarbiat Modares Univ., Tehran, Iran
Abstract :
In this paper, we have discussed about the Sliding mode Controller (SMC) for missile autopilot. The chattering phenomenon has been studied as the main problem of these systems; we use boundary layer method to overcome this problem. Therefore, the system is robust under various uncertainties and external disturbances. Also, the stability of the system is proved by the Lyapunov theory. In following, Fuzzy control is applied to calculate the controller gain (k), which is responsible for stability.
Keywords :
Lyapunov methods; automatic guided vehicles; control system synthesis; fuzzy control; missile control; stability; variable structure systems; Lyapunov theory; boundary layer method; chattering phenomenon; controller gain; fuzzy sliding mode control; missile autopilot design; Force; Fuzzy control; Missiles; Sliding mode control; Trajectory; Uncertainty; Autopilot; Ballistic missile; Fuzzy control; Siding mode control; chattering phenomenon;
Conference_Titel :
GCC Conference and Exhibition (GCC), 2011 IEEE
Conference_Location :
Dubai
Print_ISBN :
978-1-61284-118-2
DOI :
10.1109/IEEEGCC.2011.5752563
