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Real time fault tolerant nonlinear attitude control system for nanosatellite applications

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Figure

Table 3.2nd SMC Controller Parameters
Figure 2.Quaternion Tracking Error and Wheel Torques Results using AFSMC controller: t=70s, Actuator Fault;t=80s, Actuator noise
Figure 3.Wheel Voltage, Wheel Speed and Wheel Torques Fault Tolerance Results using AFSMC Controller: t=70s,Actuator Fault; t=80s, Actuator noise
Figure 4.Quaternion Tracking Error, Angular Velocity Tracking Error Fault Tolerance Results using 2nd SMC Con-troller and 3rd SMC Controller : t=70s, Actuator Fault; t=80s, Actuator noise
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