Research Article

Improved Adaptive Fault-Tolerant Control of a Variable Structure Fighter with Multiple Faults Based on an Extended Observer

Figure 4

Fault estimation of rudder LIP fault. (a) Superimposed deviation fault of aileron δa. (b) Superimposed deviation fault of yaw rudder δr. (c) Superimposed deviation fault of elevator δe.
(a)
(b)
(c)