Open access
2026
Adaptive Fixed-Time Fault Tolerant Control for Rigid Spacecraft Under Harsh Conditions: Simultaneous Actuator and Sensor Faults
In-orbit operation of rigid spacecraft fundamentally relies on attitude tracking control. However, tracking performance is highly dependent on the reliability of onboard actuators and sensors, and it can be significantly degraded, or even fail, if any actuator or sensor becomes faulty. The consequences may become more...
Xuan Mung Nguyen, Gyeong Min Kim, Heeseok Shin et al.
· IEEE Access · 0 citations