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Optimal Input Design for Aircraft Stability and Control Flight Testing

Published Online: 2021-10-20

Published Print: 2021-12

Authors

Morelli, Eugene A. https://orcid.org/0000-0002-6500-1771
Funding

Funding for this research was provided by:

NASA Aeronautics Research Mission Directorate (ARMD) Transformational Tools and Technologies (TTT) project
License Information

Text and Data Mining valid from 2021-10-20

Version of Record valid from 2021-10-20
More Information

Article History

Received: 17 September 2020

Accepted: 14 July 2021

First Online: 20 October 2021

Document is current