In-flight system identification

Author:

Morelli Eugene1

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Cited by 23 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. Optimal Input Design for Aircraft Stability and Control Flight Testing;Journal of Optimization Theory and Applications;2021-10-20

2. Practical Aspects of Multiple-Input Design for Aircraft System Identification Flight Tests;AIAA AVIATION 2021 FORUM;2021-07-28

3. Lateral‐ D irectional Stability;Introduction to Flight Testing;2021-05-21

4. VIRTTAC - A Family of Virtual Test Aircraft for Use in Flight Mechanics and GNC Benchmarks;AIAA Scitech 2019 Forum;2019-01-06

5. Aircraft System Identification Using Artificial Neural Networks;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

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