Flight Test of an Adaptive Configuration Optimization System for Transport Aircraft
Title | Flight Test of an Adaptive Configuration Optimization System for Transport Aircraft PDF eBook |
Author | Glenn B. Gilyard |
Publisher | |
Pages | 20 |
Release | 1999 |
Genre | Ailerons |
ISBN |
Flight Test of an Adaptive Configuration Optimization System for Transport Aircraft
Title | Flight Test of an Adaptive Configuration Optimization System for Transport Aircraft PDF eBook |
Author | Glenn B. Gilyard |
Publisher | |
Pages | 12 |
Release | 1999 |
Genre | Ailerons |
ISBN |
FLIGHT TEST OF AN ADAPTIVE CONFIGURATION OPTIMIZATION SYSTEM FOR TRANSPORT AIRCRAFT... NASA/TM-1999-206569... MAR. 1, 1999
Title | FLIGHT TEST OF AN ADAPTIVE CONFIGURATION OPTIMIZATION SYSTEM FOR TRANSPORT AIRCRAFT... NASA/TM-1999-206569... MAR. 1, 1999 PDF eBook |
Author | United States. National Aeronautics and Space Administration |
Publisher | |
Pages | |
Release | 1999* |
Genre | |
ISBN |
Flight Test of an Adaptive Configuration System for Transport Aircraft
Title | Flight Test of an Adaptive Configuration System for Transport Aircraft PDF eBook |
Author | Glenn B. Gilyard |
Publisher | |
Pages | |
Release | 1999 |
Genre | |
ISBN |
Development of a Real-time Transport Performance Optimization Methodology
Title | Development of a Real-time Transport Performance Optimization Methodology PDF eBook |
Author | Glenn Gilyard |
Publisher | |
Pages | 22 |
Release | 1996 |
Genre | Aerodynamics |
ISBN |
A Concept for Adaptive Performance Optimization on Commercial Transport Aircraft
Title | A Concept for Adaptive Performance Optimization on Commercial Transport Aircraft PDF eBook |
Author | National Aeronautics and Space Administration (NASA) |
Publisher | Createspace Independent Publishing Platform |
Pages | 68 |
Release | 2018-07-02 |
Genre | |
ISBN | 9781722129736 |
An adaptive control method is presented for the minimization of drag during flight for transport aircraft. The minimization of drag is achieved by taking advantage of the redundant control capability available in the pitch axis, with the horizontal tail used as the primary surface and symmetric deflection of the ailerons and cruise flaps used as additional controls. The additional control surfaces are excited with sinusoidal signals, while the altitude and velocity loops are closed with guidance and control laws. A model of the throttle response as a function of the additional control surfaces is formulated and the parameters in the model are estimated from the sensor measurements using a least squares estimation method. The estimated model is used to determine the minimum drag positions of the control surfaces. The method is presented for the optimization of one and two additional control surfaces. The adaptive control method is extended to optimize rate of climb with the throttle fixed. Simulations that include realistic disturbances are presented, as well as the results of a Monte Carlo simulation analysis that shows the effects of changing the disturbance environment and the excitation signal parameters. Jackson, Michael R. and Enns, Dale F. Unspecified Center...
A Concept for Adaptive Performance Optimization on Commercial Transport Aircraft
Title | A Concept for Adaptive Performance Optimization on Commercial Transport Aircraft PDF eBook |
Author | |
Publisher | |
Pages | 72 |
Release | 1995 |
Genre | |
ISBN |