This paper contains a simulation study of a real-time adaptive least-squares drag minimization algorithm for an aeroelastic model of a flexible wing aircraft. The aircraft model is based on the NASA Generic Transport Model (GTM). The wing structures incorporate a novel aerodynamic control surface known as the Variable Camber Continuous Trailing Edge Flap (VCCTEF). The drag minimization algorithm uses the Newton-Raphson method to find the optimal VCCTEF deflections for minimum drag in the context of an altitude-hold flight control mode at cruise conditions. The aerodynamic coefficient parameters used in this optimization method are identified in real-time using Recursive Least Squares (RLS). The results demonstrate the potential of the VCCTE...
This paper presents a coupled vortex-lattice flight dynamic model with an aeroelastic finite-element...
A real-time optimization strategy can provide any system with a considerable boost in performance on...
This paper considers the control of coupled aeroelastic aircraft model with Variable Camber Continuo...
In this paper, we describe an initial optimization study of a Variable-Camber Continuous Trailing-Ed...
This paper reports the results of a recently completed real-time adaptive drag minimization wind tun...
This paper summarizes the recent development of an adaptive aeroelastic wing shaping control technol...
This paper presents experimental results of a flexible wing wind tunnel model with a variable camber...
Boeing and NASA are conducting a joint study program to design a wing flap system that will provide ...
This paper reports a detailed computational high-lift study of the Variable Camber Continuous Traili...
Lightweight aircraft design has received a considerable attention in recent years as a means for imp...
An overview of recent aeroelasitc wing-shaping work at the NASA Ames Research Center is presented. T...
A direct optimization study was performed to produce a preliminary evaluation of the potential benef...
Optimal control settings (camber scheduling) can be used by aircraft to minimize drag at various ope...
The practical application of real-time performance optimization is addressed (using a wide-body tran...
This paper presents data analysis of a flexible wing wind tunnel model with a variable camber contin...
This paper presents a coupled vortex-lattice flight dynamic model with an aeroelastic finite-element...
A real-time optimization strategy can provide any system with a considerable boost in performance on...
This paper considers the control of coupled aeroelastic aircraft model with Variable Camber Continuo...
In this paper, we describe an initial optimization study of a Variable-Camber Continuous Trailing-Ed...
This paper reports the results of a recently completed real-time adaptive drag minimization wind tun...
This paper summarizes the recent development of an adaptive aeroelastic wing shaping control technol...
This paper presents experimental results of a flexible wing wind tunnel model with a variable camber...
Boeing and NASA are conducting a joint study program to design a wing flap system that will provide ...
This paper reports a detailed computational high-lift study of the Variable Camber Continuous Traili...
Lightweight aircraft design has received a considerable attention in recent years as a means for imp...
An overview of recent aeroelasitc wing-shaping work at the NASA Ames Research Center is presented. T...
A direct optimization study was performed to produce a preliminary evaluation of the potential benef...
Optimal control settings (camber scheduling) can be used by aircraft to minimize drag at various ope...
The practical application of real-time performance optimization is addressed (using a wide-body tran...
This paper presents data analysis of a flexible wing wind tunnel model with a variable camber contin...
This paper presents a coupled vortex-lattice flight dynamic model with an aeroelastic finite-element...
A real-time optimization strategy can provide any system with a considerable boost in performance on...
This paper considers the control of coupled aeroelastic aircraft model with Variable Camber Continuo...
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