The practical application of real-time performance optimization is addressed (using a wide-body transport simulation) based on real-time measurements and calculation of incremental drag from forced response maneuvers. Various controller combinations can be envisioned although this study used symmetric outboard aileron and stabilizer. The approach is based on navigation instrumentation and other measurements found on state-of-the-art transports. This information is used to calculate winds and angle of attack. Thrust is estimated from a representative engine model as a function of measured variables. The lift and drag equations are then used to calculate lift and drag coefficients. An expression for drag coefficient, which is a function of pa...
Conventional Mach-independent subsonic drag polar does not replicate the real airplane drag characte...
A peak-seeking control algorithm for real-time trim optimization for reduced fuel consumption has be...
Aircraft performance can be optimized at the flight condition by using available redundancy among ac...
A flight research program exploring the practical application of real-time performance optimization ...
Increasing competition among airline manufacturers and operators has highlighted the issue of aircra...
An adaptive control method is presented for the minimization of drag during flight for transport air...
This thesis focuses on the use of multiple redundant control surfaces to increase performance during...
This paper contains a simulation study of a real-time adaptive least-squares drag minimization algor...
A technique was developed which permits simultaneous extraction of complete lift, drag, and thrust p...
This paper reports the results of a recently completed real-time adaptive drag minimization wind tun...
Two methods for constructing performance functions for formation fight-for-drag-reduction suitable f...
A peak-seeking control approach for real-time trim configuration optimization for reduced fuel consu...
A real-time optimization strategy can provide any system with a considerable boost in performance on...
A direct optimization study was performed to produce a preliminary evaluation of the potential benef...
The purpose of this study was to determine if advanced supercritical wings incur higher trim drag va...
Conventional Mach-independent subsonic drag polar does not replicate the real airplane drag characte...
A peak-seeking control algorithm for real-time trim optimization for reduced fuel consumption has be...
Aircraft performance can be optimized at the flight condition by using available redundancy among ac...
A flight research program exploring the practical application of real-time performance optimization ...
Increasing competition among airline manufacturers and operators has highlighted the issue of aircra...
An adaptive control method is presented for the minimization of drag during flight for transport air...
This thesis focuses on the use of multiple redundant control surfaces to increase performance during...
This paper contains a simulation study of a real-time adaptive least-squares drag minimization algor...
A technique was developed which permits simultaneous extraction of complete lift, drag, and thrust p...
This paper reports the results of a recently completed real-time adaptive drag minimization wind tun...
Two methods for constructing performance functions for formation fight-for-drag-reduction suitable f...
A peak-seeking control approach for real-time trim configuration optimization for reduced fuel consu...
A real-time optimization strategy can provide any system with a considerable boost in performance on...
A direct optimization study was performed to produce a preliminary evaluation of the potential benef...
The purpose of this study was to determine if advanced supercritical wings incur higher trim drag va...
Conventional Mach-independent subsonic drag polar does not replicate the real airplane drag characte...
A peak-seeking control algorithm for real-time trim optimization for reduced fuel consumption has be...
Aircraft performance can be optimized at the flight condition by using available redundancy among ac...