Publicación: A New Pitch Angle Adaptive Control Design
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2014-06-26
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info:eu-repo/semantics/openAccess
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IEEE
Resumen
This paper presents a new pitch angle adaptive control design based on the pitch rate following of a desired trajectory that ensures closed loop satisfactory performance. The pitch rate is under adaptive predictive (AP) control, as previously seen in the literature, but its desired trajectory is produced by a guidance block within a global guidance system structure that ensures automatic pitch angle closed loop performance. Additionally, the guidance block presented in this paper allows satisfactory operation of the automatic pilot in a range of high control frequencies suitable for this kind of application, overcoming stability problems that may arise within these high frequencies by direct application of a pitch angle AP controller. Experimental results obtained by flying a simulated aircraft illustrate comparatively the guidance system performance, and show the robustness of the new design with aerodynamic disturbances.
Descripción
The registered version, published in “2014 International Conference on Unmanned Aircraft Systems, ICUAS 2014 - Conference Proceedings", is available online at the publisher's website: https://doi.org/10.1109/ICUAS.2014.6842342
Categorías UNESCO
Palabras clave
Pitch Angle Control, Optimized Adaptive Control, Adaptive Predictive Control, Derivative Control, Guidance System
Citación
Viúdez-Moreiras, D., Martin, I., Martín-Sánchez J.M. (2014) “A New Pitch Angle Adaptive Control Design”. IEEE International Conference on Unmanned Aircraft Systems 2014, Orlando, Florida, USA, May 2014. pp. 928-935, ISBN: 978-1-4799-2376-2. https://doi.org/10.1109/ICUAS.2014.6842342
Centro
Facultades y escuelas::E.T.S. de Ingenieros Industriales
Departamento
Ingeniería Eléctrica, Electrónica, Control, Telemática y Química Aplicada a la Ingeniería