Newtonian Development of the Mean-Axis Reference Frame for Flexible Aircraft-Reference-Cited by-同舟云学术

Newtonian Development of the Mean-Axis Reference Frame for Flexible Aircraft

Published:2019-01 Issue:1 Volume:56 Page:392-397
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Keyes Sally Ann¹,Seiler Peter¹,Schmidt David K.²

Affiliation:

1. University of Minnesota, Minneapolis, Minnesota 55455

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

Funder

National Aeronautics and Space Administration

College of Science and Engineering, University of Minnesota

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C035041

Reference13 articles.

1. MilneR. D. “Dynamics of the Deformable Aeroplane,” Aeronautical Research Council Repts. and Memoranda No. 3345, London, 1964, http://naca.central.cranfield.ac.uk/reports/arc/rm/3345.pdf [retrieved 2018].

2. Nonlinear simulation of a flexible aircraft in maneuvering flight

3. Flight-Dynamics and Flutter Modeling and Analyses of a Flexible Flying-Wing Drone - Invited

4. ReschkeC. “Integrated Flight Loads Modelling and Analysis for Flexible Transport Aircraft,” Ph.D. Thesis, Univ. of Stuttgart, Stuttgart, Germany, 2005.

5. Robust Control Design for Active Flutter Suppression

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