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Development of a real-time transport performance optimization methodologyThe 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 parasite drag, induced drag, and aileron drag, is solved from forced excitation response data. Estimates of the parasite drag, curvature of the aileron drag variation, and minimum drag aileron position are produced. Minimum drag is then obtained by repositioning the symmetric aileron. Simulation results are also presented which evaluate the affects of measurement bias and resolution.
Document ID
19960014807
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Gilyard, Glenn
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1996
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA-TM-4730
AIAA Paper 96-0093
NAS 1.15:4730
H-2085
Report Number: NASA-TM-4730
Report Number: AIAA Paper 96-0093
Report Number: NAS 1.15:4730
Report Number: H-2085
Accession Number
96N21251
Funding Number(s)
PROJECT: RTOP 505-64-10-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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