Fault-tolerant control for a Multi-propeller Aerostat based on sliding mode control allocation method

Author(s):  
K.K. Liang ◽  
L. Chen ◽  
J.G. Liu
Author(s):  
Majied Mokhtari ◽  
Mostafa Taghizadeh ◽  
Pegah Ghaf Ghanbari

In this paper, an active fault-tolerant control scheme is proposed for a lower limb exoskeleton, based on hybrid backstepping nonsingular fast terminal integral type sliding mode control and impedance control. To increase the robustness of the sliding mode controller and to eliminate the chattering, a nonsingular fast terminal integral type sliding surface is used, which ensures finite time convergence and high tracking accuracy. The backstepping term of this controller guarantees global stability based on Lyapunov stability criterion, and the impedance control reduces the interaction forces between the user and the robot. This controller employs a third order super twisting sliding mode observer for detecting, isolating ad estimating sensor and actuator faults. Motion stability based on zero moment point criterion is achieved by trajectory planning of waist joint. Furthermore, the highest level of stability, minimum error in tracking the desired joint trajectories, minimum interaction force between the user and the robot, and maximum system capability to handle the effect of faults are realized by optimizing the parameters of the desired trajectories, the controller and the observer, using harmony search algorithm. Simulation results for the proposed controller are compared with the results obtained from adaptive nonsingular fast terminal integral type sliding mode control, as well as conventional sliding mode control, which confirm the outperformance of the proposed control scheme.


2009 ◽  
Vol 42 (8) ◽  
pp. 265-270 ◽  
Author(s):  
H. Alwi ◽  
C. Edwards ◽  
O. Stroosma ◽  
J.A. Mulder

2018 ◽  
Vol 28 (8) ◽  
pp. 3015-3032 ◽  
Author(s):  
Ahmadreza Argha ◽  
Steven W. Su ◽  
Andrey Savkin ◽  
Branko G. Celler

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