Modeling, Design, and Flight Testing of Three Flutter Controllers for a Flying-Wing Drone-Reference-Cited by-同舟云学术

Modeling, Design, and Flight Testing of Three Flutter Controllers for a Flying-Wing Drone

Published:2020-07 Issue:4 Volume:57 Page:615-634
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Schmidt David K.¹,Danowsky Brian P.,Kotikalpudi Aditya,Theis Julian²,Regan Christopher D.,Seiler Peter J.,Kapania Rakesh K.³

Affiliation:

1. D. K. Schmidt and Associates, Monument, Colorado 80132

2. Hamburg University of Technology, 21073 Hamburg, Germany

3. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24060

Funder

Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.C035720

Reference57 articles.

1. Active Flutter Suppression-A Flight Test Demonstration

2. WykesJ. H.BorlandC. J.KleplM. J.MacMillerC. J. “Design and Development of a Structural Mode Control System,” NASA CR-143846, Prepared by Rockwell International, Inc. Oct. 1977.

3. NewsomJ. R.AbelI.DunnH. J. “Application of Two Design Methods for Active Flutter Suppression and Wind-Tunnel Test Results,” NASA TP 1653, May 1980.

4. Aircraft Active Flutter Suppression: State of the Art and Technology Maturation Needs

5. Aircraft Design and Testing of FLEXOP Unmanned Flying Demonstrator to Test Load Alleviation and Flutter Suppression of High Aspect Ratio Flexible Wings

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