This paper presents a summary of the NASA/Rockwell Active Flexible Wing program. Major elements of the program are presented. Key program accomplishments included single- and multiple-mode flutter suppression, load alleviation and load control during rapid roll maneuvers, and multi-input/multi-ouput multiple-function active controls tests above the open-loop flutter boundary.
A summary of the Active Flexible Wing program
AIAA Dynamics Specialists Conference ; 1992 ; Dallas, TX, United States
1992-01-01
Conference paper
No indication
English
Summary of an Active Flexible Wing program
AIAA | 1995
|Summary of an Active Flexible Wing Program
Online Contents | 1995
|Summary of the Active Flexible Wing Program
NTIS | 1992
|A summary of the active flexible wing program
NTRS | 1992
|A summary of the Active Flexible Wing program
AIAA | 1992
|