Mathematical Problems in Engineering / 2014 / Article / Fig 6

Research Article

Direct Self-Repairing Control for Quadrotor Helicopter Attitude Systems

Figure 6

The output response curves with the loss of effectiveness in .
187345.fig.006a
(a) Rolling angle tracking curves
187345.fig.006b
(b) Pitching angle tracking curves
187345.fig.006c
(c) Yawing angle tracking curves