Trajectory Tracking Control of a PVTOL Aircraft Based on Linear Algebra Theory
In this work, a trajectory tracking control design is proposed for the planar vertical takeoff and landing (PVTOL) aircraft using linear algebra theory. The resulting control law is implemented easily since the equation to be solved is not complex. The tracking is achieved providing convergence of t...
| Autores: | , , , , |
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| Formato: | artículo |
| Estado: | Versión publicada |
| Fecha de publicación: | 2014 |
| País: | Argentina |
| Recursos: | Consejo Nacional de Investigaciones Científicas y Técnicas |
| Repositorio: | CONICET Digital (CONICET) |
| Idioma: | inglés |
| OAI Identifier: | oai:ri.conicet.gov.ar:11336/12563 |
| Acesso em linha: | http://hdl.handle.net/11336/12563 |
| Access Level: | acceso abierto |
| Palavra-chave: | Pvtol Aircraft Markov Propriety Linear Algebra Based Controller Internal States Tracking Error https://purl.org/becyt/ford/2.2 https://purl.org/becyt/ford/2 |
| Resumo: | In this work, a trajectory tracking control design is proposed for the planar vertical takeoff and landing (PVTOL) aircraft using linear algebra theory. The resulting control law is implemented easily since the equation to be solved is not complex. The tracking is achieved providing convergence of the tracking errors to zero, and simulation results show the good performance of the proposed controller. |
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