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Fault Diagnosis and Fault-Tolerant Control of Unmanned Aerial Vehicles

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Academic year: 2021

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Figure

Figure 1.3: The fundamental architecture of a typical UAV system.
Figure 3.4: Control input of the faulty actuator using nominal SMC with 20% loss of control effectiveness in actuator #1
Figure 3.6: Control input of the faulty actuator using adaptive SMC with 20% loss of control effectiveness in actuator #1
Figure 3.9: Control input of the faulty actuator using nominal SMC with 50% loss of control effectiveness in actuator #1
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