Schmidt, David2015-06-302015-06-302015-06-15https://hdl.handle.net/11299/172717Included is a presentation given by David Schmidt of Schmidt and Associates at the NASA Armstrong Flight Research Center. This presentation discussed the Flight Dynamics approach to modeling flexible vehicles and the Identically Located Acceleration and Force (ILAF) control law synthesis. Results for the Lockheed Martin Free Flight Aeroelastic Demonstrator (FFAD) vehicle were shown.enFlight Dynamics ModelIdentically Located Acceleration and ForceILAFFlutter SuppressionFlexible Vehicle ModelingControl Law SynthesisFlight-Dynamics, Flutter, and Active-Flutter-Suppression Analyses of a Flexible Flying-Wing Research DronePresentation