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Development of an Aeroservoelastic Model for Gust Load Alleviation of the NASA Common Research Model Wind Tunnel ExperimentAs aircraft move to using composite materials as their primary structure they become lighter and more flexible as well. This presents some significant challenges in association with gust load alleviation. In this paper we develop an aeroservoelastic model for use in developing controllers that utilize distributed control surfaces for active gust load alleviation in a set of wind tunnel experiments. The model is based on an preexisting aeroelastic wing tunnel model and compares the baseline functionality to it. We also provide simple full state feedback simulations for the model.
Document ID
20200000327
Acquisition Source
Ames Research Center
Document Type
Conference Paper
External Source(s)
doi:10.2514/6.2020-0211
Authors
Cramer, Nick (NASA Ames Research Center Moffett Field, CA, United States)
Nguyen, Nhan (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
January 16, 2020
Publication Date
January 6, 2020
Subject Category
Aerodynamics
Report/Patent Number
AIAA 2020-0211
ARC-E-DAA-TN76375
Meeting Information
Meeting: AIAA Scitech 2020 Forum
Location: Orlando, FL
Country: United States
Start Date: January 6, 2020
End Date: January 10, 2020
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
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