Publication Date:
2019-07-20
Description:
These slides describe a method and technology of modeling flexible aircraft for active control of structural dynamics. Objective: Generate models useful for the design and evaluation of control laws for active structural control and flutter suppression that are able to accurately predict body freedom flutter.
Keywords:
Aircraft Stability and Control
Type:
AFRC-E-DAA-TN66921
,
Aerospace Control and Guidance Systems Committee (ACGSC) Meeting; Mar 27, 2019 - Mar 29, 2019; Santa Fe, NM; United States
Format:
application/pdf