“…The step command is used as the attitude angle command to analyze the effect of command parameters on the performance of the system, without considering the influence of deviations in aerodynamic parameters and disturbances. In addition, the controller parameters are given as k 1 = diag (15,5), k 2 = diag (20,10) and the command parameters are given as K p , K r = 10, 20, 35, 60, respectively.…”