Aircraft Dutch Roll and State Variables Analysis Using Yaw Damper and Washout Filter
Aircraft Dutch Roll and State Variables Analysis Using Yaw Damper and Washout Filter

Emad N. Abdulwahab

Volume 27, Issue 7 , May 2009, , Page 1351-1369

https://doi.org/10.30684/etj.27.7.11

Abstract
  Many high performance aircraft suffer from a dynamic instability problem at relativelyhigh Mach number and altitude regimes known as Dutch roll instability. In this study theaircraft ...  Read More ...