This paper presents a comparative study of various control allocation methods, using ADMIRE as a benchmark simulation model. The Ganged Pseudo-Inverse, Weighted Pseudo-Inverse, Cascaded Generalized-Inverse, Daisy Chain, and Linear Programming approaches are evaluated and compared against each other using open loop and closed loop analysis with Euclidean-Norm. In open-loop analysis, control allocation methods are analyzed for each approach that can produce an admissible solution and be able to attain commanded moments. Then, in closed-loop analysis, control allocation methods are compared using ADMIRE nonlinear simulation model for predefined maneuvers which are defined by multiple points in the flight envelope
Following extensive development over the past two decades, techniques of inverse simulation have led...
DESIGN of maneuvers for carefree access of an aircraft to its complete flight envelope including pos...
Methods for allocating redundant controls for systems with four or more objectives are studied. Prev...
The forces and moments produced by a vehicle's aerodynamic control surfaces are often nonlinear func...
Conventional linear control allocation (LCA) methods fail to provide satisfactory performance in fli...
The modern trend of developing highly automated aircraft is characterized by a transition from tradi...
International audienceTo achieve a high performance level during ground operations, the lateral dyna...
This dissertation aims at F-16 fighter to design controller and to make simulation for analyzing its...
The objective of the present dissertation is to show how redundant control surfaces can be exploited...
A nonlinear flight controller is developed using dynamic inversion principles. The nonlinearities in...
This paper contains a study of two methods for use in a generic nonlinear simulation tool that could...
An inverse simulation can be used to find system inputs such that model outputs will match specified...
This paper describes the maturation of a control allocation technique designed to assist pilots in r...
This thesis presents an automated design methodology for development of six degree-of-freedom aircra...
This report documents the application of the inverse simulation algorithm Genisa [1] to the Concept...
Following extensive development over the past two decades, techniques of inverse simulation have led...
DESIGN of maneuvers for carefree access of an aircraft to its complete flight envelope including pos...
Methods for allocating redundant controls for systems with four or more objectives are studied. Prev...
The forces and moments produced by a vehicle's aerodynamic control surfaces are often nonlinear func...
Conventional linear control allocation (LCA) methods fail to provide satisfactory performance in fli...
The modern trend of developing highly automated aircraft is characterized by a transition from tradi...
International audienceTo achieve a high performance level during ground operations, the lateral dyna...
This dissertation aims at F-16 fighter to design controller and to make simulation for analyzing its...
The objective of the present dissertation is to show how redundant control surfaces can be exploited...
A nonlinear flight controller is developed using dynamic inversion principles. The nonlinearities in...
This paper contains a study of two methods for use in a generic nonlinear simulation tool that could...
An inverse simulation can be used to find system inputs such that model outputs will match specified...
This paper describes the maturation of a control allocation technique designed to assist pilots in r...
This thesis presents an automated design methodology for development of six degree-of-freedom aircra...
This report documents the application of the inverse simulation algorithm Genisa [1] to the Concept...
Following extensive development over the past two decades, techniques of inverse simulation have led...
DESIGN of maneuvers for carefree access of an aircraft to its complete flight envelope including pos...
Methods for allocating redundant controls for systems with four or more objectives are studied. Prev...