Flight-Dynamics, Flutter, and Active-Flutter-Suppression Analyses of a Flexible Flying-Wing Research Drone

Schmidt, David
2015-06-15
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https://hdl.handle.net/11299/172717
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Flight-Dynamics, Flutter, and Active-Flutter-Suppression Analyses of a Flexible Flying-Wing Research Drone

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2015-06-15

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As presented at the NASA Armstrong Flight Research Center Edwards AFB, CA

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Included 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.

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NASA NRA, "Lightweight Adaptive Aeroelastic Wing for Enhanced Performance Across the Flight Envelope," NRA NNX14AL36A, Mr. John Bosworth Technical Monitor.

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Schmidt, David. (2015). Flight-Dynamics, Flutter, and Active-Flutter-Suppression Analyses of a Flexible Flying-Wing Research Drone. Retrieved from the University Digital Conservancy, https://hdl.handle.net/11299/172717.

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