Assessing Aircraft Susceptibility to Nonlinear Aircraft-Pilot Coupling/Pilot-Induced Oscillations
Open Access
- 1 November 1998
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 21 (6) , 957-964
- https://doi.org/10.2514/2.4330
Abstract
No abstract availableKeywords
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- Flight test evaluation of techniques to predict longitudinal pilot induced oscillationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986