Mendeley
TY  _  JOUR
ID  -  1394083012151431
TI  -  Missile Autopilot Design Using Fuzzy Gain-Scheduling
JO  -  Nashriyyah -i Muhandisi -i Barq va Muhandisi -i Kampyutar -i Iran
JA  -  ES
LA  -  fa
SN  -  16823745
AU  -  Akbarzadeh Kalat A.
AU  -  momeni hamidreza
AD  -  دانشگاه تربيت مدرس
AD  -  
Y1  -  2007
PY  -  2007
VL  -  2
IS  -  
SP  -  59
EP  -  68
KW  -  Fuzzy gain-schedulingautopilotaerodynamic coefficientsgenetic algorithmlinear least squares
DO  -  
N2  -  In this paper a controller using fuzzy gain-scheduling for the channels of a tactical missile is designed such that in flight trajectories, performance is achieved. In this design method, the fuzzy gain-scheduling zone centers are determined by a training algorithm according to dynamic pressure, Mach number and coefficients of linear model of system in major operating points. The fuzzy system is learned using combined genetic and linear least squares algorithms. In this manner both global optimum solution and fast convergence are reachable. Moreover the membership functions in fuzzy inference system are chosen with special and suitable properties, which cause simple and effective scheduling process. Performance of this method is shown with case study simulation result.
UR  - rimag.ir/en/Article/27867
L1  - rimag.ir/en/Article/Download/27867
ER  -  
