Adaptive Energy Control of Longitudinal Aircraft Dynamics
dc.contributor.author | Anandakumar, Ashwin | |
dc.contributor.author | Bernstein, Dennis S. | |
dc.contributor.author | Goel, Ankit | |
dc.date.accessioned | 2022-01-26T14:31:52Z | |
dc.date.available | 2022-01-26T14:31:52Z | |
dc.date.issued | 2021-12-29 | |
dc.description | AIAA SCITECH 2022 Forum January 3-7, 2022 San Diego, CA & Virtual | |
dc.description.abstract | The Total Energy Control System (TECS) is a method to control airplane longitudinal flight dynamics by regulating energy and energy balance. This multiple input, multiple output method accounts for the highly coupled nature of aircraft dynamics and allows for control of airspeed and altitude with a proportional-integral controller. This paper reviews the heuristic TECS control law and then validates it in a MATLAB simulation. Next, an adaptive TECS is designed by augmenting the fixed-gain controllers in a nominal TECS with retrospective cost optimization-based adaptive controllers. It is shown through simulations that adaptive augmentation improves the closed-loop performance and accelerates the tuning process. | en_US |
dc.description.uri | https://arc.aiaa.org/doi/abs/10.2514/6.2022-0965 | en_US |
dc.format.extent | 12 pages | en_US |
dc.genre | conference papers and proceedings | en_US |
dc.genre | postprints | en_US |
dc.identifier | doi:10.13016/m21g77-nug2 | |
dc.identifier.citation | Ashwin Anandakumar, Dennis Bernstein and Ankit Goel. "Adaptive Energy Control of Longitudinal Aircraft Dynamics," AIAA 2022-0965. AIAA SCITECH 2022 Forum. January 2022. | en_US |
dc.identifier.uri | https://doi.org/10.2514/6.2022-0965 | |
dc.identifier.uri | http://hdl.handle.net/11603/24082 | |
dc.language.iso | en_US | en_US |
dc.publisher | American Institute of Aeronautics and Astronautics | en_US |
dc.relation.isAvailableAt | The University of Maryland, Baltimore County (UMBC) | |
dc.relation.ispartof | UMBC Mechanical Engineering Department Collection | |
dc.relation.ispartof | UMBC Faculty Collection | |
dc.rights | This item is likely protected under Title 17 of the U.S. Copyright Law. Unless on a Creative Commons license, for uses protected by Copyright Law, contact the copyright holder or the author. | en_US |
dc.title | Adaptive Energy Control of Longitudinal Aircraft Dynamics | en_US |
dc.type | Text | en_US |
dcterms.creator | https://orcid.org/0000-0002-4146-6275 | en_US |