Fault-tolerant flight control has the potential of improving the aircraft survivability in real life. This paper proposes an Incremental Backstepping Sliding Mode Control (IBSMC) framework for multi-input/output nonlinear strict-feedback systems considering model uncertainties, sudden faults, and external disturbances. This approach is a hybridization of the Sliding Mode Control (SMC) and a reformulated Incremental Backstepping (IBS). By virtue of the benefits contributed by both SMC and IBS, theoretical analyses prove IBSMC has less model dependency and enhanced robustness as compared to backstepping and backstepping hybridized with SMC (BSMC). When applied to an aircraft fault-tolerant control problem, numerical simulations demonstrate IB...
This paper deals with aircraft trajectory control in the presence of model uncertainties and actuato...
International audienceIn this paper, an autopilot for attitude tracking is designed using disturbanc...
Presence of uncertainties caused by unforeseen malfunctions in actuation system or changes in aircra...
This paper proposes a novel control framework that combines the recently reformulated incremental no...
This paper proposes a novel control framework that combines the recently reformulated incremental no...
Copyright © 2014 Institution of Engineering and Technology (IET)This study proposes a novel non-line...
Recently, an incremental type sensor based backstepping (SBB) control approach, based on singular pe...
Recently, an incremental type sensor based backstepping (SBB) control approach, based on singular pe...
Recently, an incremental type sensor based backstepping (SBB) control approach, based on singular pe...
This paper presents an incremental backstepping sliding-mode (IBS) controller for trajectory control...
Nonlinear Dynamic Inversion (NDI) is a promising method for Fault Tolerant Flight Control. The NDI a...
Uncertainties caused by unforeseen malfunctions of the actuator or changes in aircraft behavior coul...
The thesis concerns the theoretical development and implemantation of sliding mode schemes for fault...
This paper presents an adaptive incremental nonlinear backstepping sliding-mode (INBSM) controller, ...
This paper deals with aircraft trajectory control in the presence of model uncertainties and actuato...
This paper deals with aircraft trajectory control in the presence of model uncertainties and actuato...
International audienceIn this paper, an autopilot for attitude tracking is designed using disturbanc...
Presence of uncertainties caused by unforeseen malfunctions in actuation system or changes in aircra...
This paper proposes a novel control framework that combines the recently reformulated incremental no...
This paper proposes a novel control framework that combines the recently reformulated incremental no...
Copyright © 2014 Institution of Engineering and Technology (IET)This study proposes a novel non-line...
Recently, an incremental type sensor based backstepping (SBB) control approach, based on singular pe...
Recently, an incremental type sensor based backstepping (SBB) control approach, based on singular pe...
Recently, an incremental type sensor based backstepping (SBB) control approach, based on singular pe...
This paper presents an incremental backstepping sliding-mode (IBS) controller for trajectory control...
Nonlinear Dynamic Inversion (NDI) is a promising method for Fault Tolerant Flight Control. The NDI a...
Uncertainties caused by unforeseen malfunctions of the actuator or changes in aircraft behavior coul...
The thesis concerns the theoretical development and implemantation of sliding mode schemes for fault...
This paper presents an adaptive incremental nonlinear backstepping sliding-mode (INBSM) controller, ...
This paper deals with aircraft trajectory control in the presence of model uncertainties and actuato...
This paper deals with aircraft trajectory control in the presence of model uncertainties and actuato...
International audienceIn this paper, an autopilot for attitude tracking is designed using disturbanc...
Presence of uncertainties caused by unforeseen malfunctions in actuation system or changes in aircra...