AbstractThis paper presents a reconfigurable flight control method based on face searching allocation algorithm for aircraft with multiple effectors. Besides the function of distributing the desired moments to control surfaces reasonably, face searching method is beneficial for the design of the reconfigurable control system. It can provide the biggest attainable moment subset and provide the maximum moment in any direction. The approach solves different effector failures by the solution of re-allocating the healthy effectors. With the redundancy of remaining effectors, the method can compensate the effects of the failure surfaces and still provide the same desired control input. Simulation results show that reconfigurable control system de...
In the event of a control surface failure a reconfigured control law redistributes the forces and m...
This paper proposes a control allocation method for the tracking control problem of a class of morph...
A reconfigurable control law for AFTI/F-16 aircraft with failed right half elevator, has been design...
AbstractWith control using redundant multiple control surface arrangement and large-deflection drag ...
AbstractIn this paper, we present a genetic algorithm based modular reconfigurable control strategy ...
AbstractThis paper presents an optimized reconfigurable control design methodology by separating con...
The main objective of this thesis is to design and evaluate reconfigurable flight control system aga...
This paper presents a historical overview of research in reconfigurable flight control with a focus ...
Two methods for control system reconfiguration have been investigated. The first method is a robust ...
From the perspective control practitioners, control of dynamics systems subjected to varying paramet...
Operational failure of control surfaces is one of the main reasons leading to aircraft crash. Since ...
Two methods for control system reconfiguration have been investigated. The first method is a robust ...
Methods for allocating redundant controls for systems with four or more objectives are studied. Prev...
A new scheme of robust fault-tolerant control allocation is designed for a discrete-time aerodynamic...
This paper presents the development and application of one approach to the control of aircraft with ...
In the event of a control surface failure a reconfigured control law redistributes the forces and m...
This paper proposes a control allocation method for the tracking control problem of a class of morph...
A reconfigurable control law for AFTI/F-16 aircraft with failed right half elevator, has been design...
AbstractWith control using redundant multiple control surface arrangement and large-deflection drag ...
AbstractIn this paper, we present a genetic algorithm based modular reconfigurable control strategy ...
AbstractThis paper presents an optimized reconfigurable control design methodology by separating con...
The main objective of this thesis is to design and evaluate reconfigurable flight control system aga...
This paper presents a historical overview of research in reconfigurable flight control with a focus ...
Two methods for control system reconfiguration have been investigated. The first method is a robust ...
From the perspective control practitioners, control of dynamics systems subjected to varying paramet...
Operational failure of control surfaces is one of the main reasons leading to aircraft crash. Since ...
Two methods for control system reconfiguration have been investigated. The first method is a robust ...
Methods for allocating redundant controls for systems with four or more objectives are studied. Prev...
A new scheme of robust fault-tolerant control allocation is designed for a discrete-time aerodynamic...
This paper presents the development and application of one approach to the control of aircraft with ...
In the event of a control surface failure a reconfigured control law redistributes the forces and m...
This paper proposes a control allocation method for the tracking control problem of a class of morph...
A reconfigurable control law for AFTI/F-16 aircraft with failed right half elevator, has been design...