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

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https://hdl.handle.net/11299/172119

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

Authors

Schmidt, David

Published Date

2015-04-16

Publisher

Aerospace Flutter and Dynamics Council (AFDC) Meeting, Spring 2015

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Presentation

Abstract

Keywords

Flight Dynamics Model

Identically Located Acceleration and Force

ILAF

Flutter Suppression

Flexible Vehicle Modeling

Control Law Synthesis

Description

Included is a presentation given by David Schmidt of Schmidt and Associates at the Aerospace Flutter and Dynamics Council (AFDC) spring 2015 meeting at NASA Ames 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, Mr. Dan Moerder acting Technical Monitor.

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Schmidt, David. (2015). Flight-Dynamics, Flutter, and Active-Flutter-Suppression Analysis of a Flexible Flying-Wing Research Drone. Retrieved from the University Digital Conservancy, https://hdl.handle.net/11299/172119.

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