Design and Stability Analysis of an Integrated Controller for Highly Flexible Advanced Aircraft Utilizing the Novel Nonlinear Dynamic Inversion

Design and Stability Analysis of an Integrated Controller for Highly Flexible Advanced Aircraft Utilizing the Novel Nonlinear Dynamic Inversion

<p>High performance aircraft of the future will be designed to be lighter, more maneuverable, and operate over an ever expanding flight envelope. This set of conditions will necessarily mean highly flexible vehicles operating in nonlinear regimes. A methodology proposed to better optimize th...

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Bibliographic Details
Main Author: Gregory, Irene Michelle
Format: Others
Published: 2005
Online Access:https://thesis.library.caltech.edu/2968/1/GregoryPhD0704.pdf
Gregory, Irene Michelle (2005) Design and Stability Analysis of an Integrated Controller for Highly Flexible Advanced Aircraft Utilizing the Novel Nonlinear Dynamic Inversion. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/Y6B1-ZZ55. https://resolver.caltech.edu/CaltechETD:etd-07232004-075729 <https://resolver.caltech.edu/CaltechETD:etd-07232004-075729>

Internet

https://thesis.library.caltech.edu/2968/1/GregoryPhD0704.pdf
Gregory, Irene Michelle (2005) Design and Stability Analysis of an Integrated Controller for Highly Flexible Advanced Aircraft Utilizing the Novel Nonlinear Dynamic Inversion. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/Y6B1-ZZ55. https://resolver.caltech.edu/CaltechETD:etd-07232004-075729 <https://resolver.caltech.edu/CaltechETD:etd-07232004-075729>

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