Open-Loop Stability and Closed-Loop Gust Alleviation on Flexible Aircraft Including Wake Modeling-Reference-Cited by-同舟云学术

Open-Loop Stability and Closed-Loop Gust Alleviation on Flexible Aircraft Including Wake Modeling

Published:2012-04-23 Issue: Volume: Page:
ISSN:
Container-title:53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA
language:
Short-container-title:

Author:

Murua Joseba,Palacios Rafael,Graham J.m.r.

Publisher

American Institute of Aeronautics and Astronautics

Reference76 articles.

1. 1Noll, T.E., Ishmael, S.D., Henwood, B., Perez-Davis, M.E., Tiffany, G.C., Gaier, M., Brown, J.M., andWierzbanowski, T. “Technical Findings, Lessons Learned, and Recommendations Resulting from the Helios Prototype Vehicle Mishap,” NATO/RTO AVT-145 Workshop on Design Concepts, Processes and Criteria for UAV Structural Integrity, Florence, Italy, May 2007.

2. AIAA Education Series;Hoblit F. M.,1988

3. AIAA Education Series;Lomax T. L.,1996

4. Aerospace Series;Howe D.,2004

5. Introduction to Aircraft Aeroelasticity and Loads

Cited by 12 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Proof of Concept for a Hardware-in-the-Loop Nonlinear Control Framework for Very Flexible Aircraft;AIAA Scitech 2021 Forum;2021-01-04

2. References;Active Spanwise Lift Control: A Distributed Parameter Approach;2020-08-31

3. Modal-Based Nonlinear Estimation and Control for Highly Flexible Aeroelastic Systems;AIAA Scitech 2020 Forum;2020-01-05

4. Dynamic lift measurements on an airfoil with periodic flap motion at high Reynolds number;AIAA Scitech 2019 Forum;2019-01-06

5. Multidimensional discrete gust loads of a large civil flexible aircraft;AIAA Atmospheric Flight Mechanics Conference;2017-01-05