Abstract
In this chapter, the multiobjective optimization design procedure will be used to tune the autopilot controllers for an autonomous Kadett© aircraft. For this aim, a multivariable PI controller is defined, and a many-objectives optimization instance is tackled using designer preferences.After themulticriteria decision making stage, the selected controller is implemented and evaluated in a real flight test.
Cite
CITATION STYLE
Reynoso Meza, G., Blasco Ferragud, X., Sanchis Saez, J., & Herrero Durá, J. M. (2017). Multiobjective optimization design procedure for an Aircraft’s flight control system. In Intelligent Systems, Control and Automation: Science and Engineering (Vol. 85, pp. 215–227). Kluwer Academic Publishers. https://doi.org/10.1007/978-3-319-41301-3_12
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