Mathematical Problems in Engineering / 2014 / Article / Fig 8

Research Article

Direct Self-Repairing Control for Quadrotor Helicopter Attitude Systems

Figure 8

The output response curves with the loss of effectiveness in .
187345.fig.008a
(a) Rolling angle tracking curves
187345.fig.008b
(b) Pitching angle tracking curves
187345.fig.008c
(c) Yawing angle tracking curves