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Design and Stability Analysis of an Integrated Controller for Highly Flexible Advanced Aircraft Utilizing the Novel Nonlinear Dynamic Inversion
2005 · California Institute of Technology · doctoral · Control and Dynamical Systems
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@misc{academicancestry_caltechthesis_caltechthesis_2968,
author = {{Academic Ancestry}},
title = {{Design and Stability Analysis of an Integrated Controller for Highly Flexible Advanced Aircraft Utilizing the Novel Nonlinear Dynamic Inversion: record of a thesis}},
year = {2026},
url = {https://academicancestry.org/thesis/caltechthesis/caltechthesis%3A2968},
note = {read on 2026-10-22}
}apa
Academic Ancestry. (2026, October 22). Design and Stability Analysis of an Integrated Controller for Highly Flexible Advanced Aircraft Utilizing the Novel Nonlinear Dynamic Inversion: Record of a thesis [Read on 2026-10-22]. https://academicancestry.org/thesis/caltechthesis/caltechthesis%3A2968