Digital adaptive control of a winged rocket in wide range flight conditions

Since spaceplanes have wide range flight conditions, the values of parameters of the dynamic equation are not constant Then some adaptive control methods for the spaceplanes have been proposed and digital control systems are suited for digital computers. The mathematical model of spaceplanes considering actuator dynamics become non-minimum phase system depending on values of discretizing zeros. In this paper, for a winged rocket an adaptive flight control system considering non-minimum phase characteristic is designed and the simulations are performed to verify the effectiveness of the control system.