Magazine Article

Control Derivatives of the F-18 Airplane

TBMG-7076

09/01/2002

Abstract
Content

Flight data gathered by use of the F-18 System Research Aircraft (SRA) based at Dryden Flight Research Center have been used to estimate stability and control derivatives for a baseline F-18 airplane. The data were obtained in the high-dynamic-pressure range of the F-18 flight envelope in an experiment performed in support of a future F-18 program to be devoted to the concept of the active aeroelastic wing (AAW). The AAW technology is intended to integrate aerodynamics, active controls, and aeroelasticity in such a way as to maximize the performance of the airplane. More specifically, the goal of the AAW project will be to maximize the contribution of a reduced-stiffness F-18 wing to roll-rate performance.

Meta TagsDetails
Citation
"Control Derivatives of the F-18 Airplane," Mobility Engineering, September 1, 2002.
Additional Details
Publisher
Published
Sep 1, 2002
Product Code
TBMG-7076
Content Type
Magazine Article
Language
English