Integrated Fault-Tolerant Control of an Over-Actuated Aircraft Using Optimal Control Allocation and Robust Sliding Mode Observers

Author(s):  
Karl Frederik Prochazka ◽  
Hugo Eduardo ◽  
Sebastian Rudolf Klein
Automatica ◽  
2020 ◽  
Vol 114 ◽  
pp. 108829 ◽  
Author(s):  
Lejun Chen ◽  
Christopher Edwards ◽  
Halim Alwi ◽  
Masayuki Sato

2020 ◽  
Vol 42 (11) ◽  
pp. 2011-2019
Author(s):  
Chengcheng Ma ◽  
Chunsheng Liu ◽  
Jiazhen Yao

In this paper, a new fault tolerant control scheme with control allocation is presented. The pseudo-inverse along the null-space control allocation is applied to the fault tolerant control system to handle the actuator constraints. The stability of the overall closed-loop system is proved via the small gain theory. The null-space vector is viewed as uncertainty, and is disposed by an integral sliding mode controller and a robust controller. The simulation results show that the new method can solve both failure scenarios and actuator saturation problems well.


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