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| Mouftah, Hussein T. |
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| Dugay, Fabrice |
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| Rettenmeier, Max |
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| Tomasch, Ernst | Graz |
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| Cornaggia, Greta |
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| Palacios-Navarro, Guillermo |
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| Uspenskyi, Borys V. |
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| Khan, Baseem |
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| Fediai, Natalia |
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| Derakhshan, Shadi |
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| Somers, Bart | Eindhoven |
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| Anvari, B. |
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| Kraushaar, Sabine | Vienna |
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| Kehlbacher, Ariane |
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| Das, Raj |
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| Werbińska-Wojciechowska, Sylwia |
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| Brillinger, Markus |
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| Eskandari, Aref |
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| Gulliver, J. |
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| Loft, Shayne |
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| Kud, Bartosz |
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| Matijošius, Jonas | Vilnius |
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| Piontek, Dennis |
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| Kene, Raymond O. |
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| Barbosa, Juliana |
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Luspay, Tamás
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (9/9 displayed)
- 2023Model Based Automatic Control Design for the T-FLEX Demonstrator Using RCE Environmentcitations
- 2022Model Based Automatic Control Design for the T-FLEX Demonstrator Using RCE Environment
- 2020Results of an Aeroelastically Tailored Wing on the FLEXOP Demonstrator Aircraftcitations
- 2020Parameter Varying Mode Decoupling for LPV systems
- 2019Flight control design for a highly flexible flutter demonstratorcitations
- 2019Flight control design for a highly flexible flutter demonstratorcitations
- 2019Structured Control Design for a Highly Flexible Flutter Demonstratorcitations
- 2019Baseline Flight Control System Design for an Unmanned Flutter Demonstrator
- 2018Control oriented reduced order modeling of a flexible winged aircraftcitations
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conferencepaper
Baseline Flight Control System Design for an Unmanned Flutter Demonstrator
Abstract
A comprehensive design of the baseline control and navigation system for a single-jet-engined flutter Demonstrator aircraft is presented in this paper. To facilitate the design task, a classical cascaded flight control structure is selected. Advanced robust control techniques are used to design and tune the individual feedback loops of the control system. Therefore, the design problems are posted as multi-objective non-linear optimization problems which are solved using non-smooth optimization techniques. The developed control system enables augmented and fully automated flights. The availability of a high-fidelity non-linear simulator allows the assessment of the flight controller performance and robustness. The control system is verified in realistic simulation scenarios along the test pattern defined for the real flight test campaign.
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