To address the control allocation problem caused by the redundant arrangement of control surfaces with nonlinear effectiveness for tailless aircraft, a novel multiobjective incremental control allocation (MICA) strategy is proposed. Firstly, the incremental nonlinear control allocation (INCA) method together with the active set quadratic programming algorithm is adopted to precisely allocate the virtual control commands. Secondly, a series of normalized objective functions in the form of increment are designed. Combining these functions by means of linear weighted sum, an incremental multiobjective function is constructed. Then, an improved nondominated sorting genetic algorithm (INSGA) is introduced to offline determine a set of weights th...
This paper introduces a Montecarlo Genetic Algorithm, hierarchical, multiobjective optimization of a...
A flight control system for a tilt rotor UAV has been synthesized based on an incremental nonlinear ...
A flight control system for a tilt rotor UAV has been synthesized based on an incremental nonlinear ...
Conventional linear control allocation (LCA) methods fail to provide satisfactory performance in fli...
The Innovative Control Effector model is a tailless delta-wing aircraft concept equipped with 11 con...
Parsifal is a box-wing aircraft with redundant control surfaces that is expected to save fuel during...
AbstractIn this paper, we present a genetic algorithm based modular reconfigurable control strategy ...
Incremental Nonlinear Dynamic Inversion provides a high performance attitude controller for multi-ro...
Controlling over-actuated Unmanned Aerial Vehicle (UAV) is an important task to achieve reliable fai...
Hybrid UAVs have gained a lot of interest for their combined vertical take-off & landing (VTOL) ...
Methods for allocating redundant controls for systems with four or more objectives are studied. Prev...
The paper seeks to study the control system design of a novel unmanned aerial vehicle (UAV). The UAV...
This paper proposes a nonlinear control architecture for flexible aircraft simultaneous trajectory t...
A self-learning adaptive flight control design for non-linear systems allows reliable and effective ...
High performance flight control systems based on the nonlinear dynamic inversion (NDI) principle req...
This paper introduces a Montecarlo Genetic Algorithm, hierarchical, multiobjective optimization of a...
A flight control system for a tilt rotor UAV has been synthesized based on an incremental nonlinear ...
A flight control system for a tilt rotor UAV has been synthesized based on an incremental nonlinear ...
Conventional linear control allocation (LCA) methods fail to provide satisfactory performance in fli...
The Innovative Control Effector model is a tailless delta-wing aircraft concept equipped with 11 con...
Parsifal is a box-wing aircraft with redundant control surfaces that is expected to save fuel during...
AbstractIn this paper, we present a genetic algorithm based modular reconfigurable control strategy ...
Incremental Nonlinear Dynamic Inversion provides a high performance attitude controller for multi-ro...
Controlling over-actuated Unmanned Aerial Vehicle (UAV) is an important task to achieve reliable fai...
Hybrid UAVs have gained a lot of interest for their combined vertical take-off & landing (VTOL) ...
Methods for allocating redundant controls for systems with four or more objectives are studied. Prev...
The paper seeks to study the control system design of a novel unmanned aerial vehicle (UAV). The UAV...
This paper proposes a nonlinear control architecture for flexible aircraft simultaneous trajectory t...
A self-learning adaptive flight control design for non-linear systems allows reliable and effective ...
High performance flight control systems based on the nonlinear dynamic inversion (NDI) principle req...
This paper introduces a Montecarlo Genetic Algorithm, hierarchical, multiobjective optimization of a...
A flight control system for a tilt rotor UAV has been synthesized based on an incremental nonlinear ...
A flight control system for a tilt rotor UAV has been synthesized based on an incremental nonlinear ...