Introduction.- Spacecraft Model and Control Allocation Formulation.-
Null-space based Optimal Control Allocation for Spacecraft
Stabilization.- Robust finite-time control allocation under actuator
misalignment.- Finite-Time Fault-Tolerant Spacecraft Attitude Control
and Control allocation with Torque Saturation.- Fault Tolerant Control
Allocation of Spacecraft Using Fault Detection and Diagnosis.- Extended
State Observer based Optimal Control Allocation.- Nonlinear
Proportional-Derivative Control Incorporating Closed-loop Control
Allocation.- Closed-Loop-Based Control Allocation for Spacecraft
Attitude Stabilization with Actuator Fault.- Conclusion