The present work is related to the design of the control surfaces actuation system that has been installed on a wind tunnel aeroelastic model within the GLAMOUR project. Such a scaled aircraft is equipped with two ailerons and an elevator, used to alleviate vertical gust loads. A control scheme, based on PID regulators, is taken into consideration, thanks to its simplicity. It was tuned through two different methodologies: an unfalsified frequency-based optimization and a Quantitative Feedback Theory (QFT) approach. Numerical results are presented, comparing the adopted methodologies, considering both simple input signals and realistic command profiles.
Optimal and robust design of a control surface actuation system within the GLAMOUR project
DE GASPARI, ALESSANDRO;TOFFOL, FRANCESCO;MANTEGAZZA, PAOLO;MANNARINO, ANDREA
2016-01-01
Abstract
The present work is related to the design of the control surfaces actuation system that has been installed on a wind tunnel aeroelastic model within the GLAMOUR project. Such a scaled aircraft is equipped with two ailerons and an elevator, used to alleviate vertical gust loads. A control scheme, based on PID regulators, is taken into consideration, thanks to its simplicity. It was tuned through two different methodologies: an unfalsified frequency-based optimization and a Quantitative Feedback Theory (QFT) approach. Numerical results are presented, comparing the adopted methodologies, considering both simple input signals and realistic command profiles.| File | Dimensione | Formato | |
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