Flight control design for a highly flexible flutter demonstrator

Tamás Luspay; Tamás Baár; Dániel Teubl; Bálint Vanek; Daniel Ossmann; Matthias Wüstenhagen; Manuel Pusch; Thiemo Kier; Sergio Waitman Filho; Andrea Iannelli; Andres Marcos; Mark H Lowenberg

doi:10.2514/6.2019-1817

Flight control design for a highly flexible flutter demonstrator

Tamás Luspay, Tamás Baár, Dániel Teubl, Bálint Vanek, Daniel Ossmann, Matthias Wüstenhagen, Manuel Pusch, Thiemo Kier, Sergio Waitman Filho, Andrea Iannelli, Andres Marcos, Mark H Lowenberg

Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

12 Citations (Scopus)

Abstract

The paper presents the control design approaches for the European research project FLEXOP. The ultimate goal is to develop and apply active flutter suppression and load alleviation techniques on an unmanned flying aircraft demonstrator. Due to the flexible wing of the aircraft new challenges rise for the control design: the traditional rigid body (baseline) control loops have to be augmented with flutter control laws. In our approach, the controllers are designed based on a dynamical model, which is briefly discussed first. Details of the baseline control design, as well as the two different flutter suppression algorithms are discussed in the paper. Hardware-in-the-Loop testing of the controllers are reported before the first test flights of the aircraft.

Original language	English
Title of host publication	Atmospheric Flight Mechanics Conference, AIAA SciTech Forum 2019
Publisher	American Institute of Aeronautics and Astronautics Inc. (AIAA)
DOIs	https://doi.org/10.2514/6.2019-1817
Publication status	Published - 6 Jan 2019

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Luspay, T., Baár, T., Teubl, D., Vanek, B., Ossmann, D., Wüstenhagen, M., Pusch, M., Kier, T., Waitman Filho, S., Iannelli, A., Marcos, A., & Lowenberg, M. H. (2019). Flight control design for a highly flexible flutter demonstrator. In Atmospheric Flight Mechanics Conference, AIAA SciTech Forum 2019 [AIAA 2019-1817] American Institute of Aeronautics and Astronautics Inc. (AIAA). https://doi.org/10.2514/6.2019-1817

Luspay, Tamás ; Baár, Tamás ; Teubl, Dániel ; Vanek, Bálint ; Ossmann, Daniel ; Wüstenhagen, Matthias ; Pusch, Manuel ; Kier, Thiemo ; Waitman Filho, Sergio ; Iannelli, Andrea ; Marcos, Andres ; Lowenberg, Mark H. / Flight control design for a highly flexible flutter demonstrator. Atmospheric Flight Mechanics Conference, AIAA SciTech Forum 2019. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2019.

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title = "Flight control design for a highly flexible flutter demonstrator",

abstract = "The paper presents the control design approaches for the European research project FLEXOP. The ultimate goal is to develop and apply active flutter suppression and load alleviation techniques on an unmanned flying aircraft demonstrator. Due to the flexible wing of the aircraft new challenges rise for the control design: the traditional rigid body (baseline) control loops have to be augmented with flutter control laws. In our approach, the controllers are designed based on a dynamical model, which is briefly discussed first. Details of the baseline control design, as well as the two different flutter suppression algorithms are discussed in the paper. Hardware-in-the-Loop testing of the controllers are reported before the first test flights of the aircraft.",

author = "Tam{\'a}s Luspay and Tam{\'a}s Ba{\'a}r and D{\'a}niel Teubl and B{\'a}lint Vanek and Daniel Ossmann and Matthias W{\"u}stenhagen and Manuel Pusch and Thiemo Kier and {Waitman Filho}, Sergio and Andrea Iannelli and Andres Marcos and Lowenberg, {Mark H}",

year = "2019",

month = jan,

day = "6",

doi = "10.2514/6.2019-1817",

language = "English",

booktitle = "Atmospheric Flight Mechanics Conference, AIAA SciTech Forum 2019",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

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Luspay, T, Baár, T, Teubl, D, Vanek, B, Ossmann, D, Wüstenhagen, M, Pusch, M, Kier, T, Waitman Filho, S, Iannelli, A, Marcos, A & Lowenberg, MH 2019, Flight control design for a highly flexible flutter demonstrator. in Atmospheric Flight Mechanics Conference, AIAA SciTech Forum 2019., AIAA 2019-1817, American Institute of Aeronautics and Astronautics Inc. (AIAA). https://doi.org/10.2514/6.2019-1817

Flight control design for a highly flexible flutter demonstrator. / Luspay, Tamás; Baár, Tamás; Teubl, Dániel; Vanek, Bálint; Ossmann, Daniel; Wüstenhagen, Matthias; Pusch, Manuel; Kier, Thiemo; Waitman Filho, Sergio; Iannelli, Andrea; Marcos, Andres; Lowenberg, Mark H.

Atmospheric Flight Mechanics Conference, AIAA SciTech Forum 2019. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2019. AIAA 2019-1817.

Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

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AU - Luspay, Tamás

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AU - Vanek, Bálint

AU - Ossmann, Daniel

AU - Wüstenhagen, Matthias

AU - Pusch, Manuel

AU - Kier, Thiemo

AU - Waitman Filho, Sergio

AU - Iannelli, Andrea

AU - Marcos, Andres

AU - Lowenberg, Mark H

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N2 - The paper presents the control design approaches for the European research project FLEXOP. The ultimate goal is to develop and apply active flutter suppression and load alleviation techniques on an unmanned flying aircraft demonstrator. Due to the flexible wing of the aircraft new challenges rise for the control design: the traditional rigid body (baseline) control loops have to be augmented with flutter control laws. In our approach, the controllers are designed based on a dynamical model, which is briefly discussed first. Details of the baseline control design, as well as the two different flutter suppression algorithms are discussed in the paper. Hardware-in-the-Loop testing of the controllers are reported before the first test flights of the aircraft.

AB - The paper presents the control design approaches for the European research project FLEXOP. The ultimate goal is to develop and apply active flutter suppression and load alleviation techniques on an unmanned flying aircraft demonstrator. Due to the flexible wing of the aircraft new challenges rise for the control design: the traditional rigid body (baseline) control loops have to be augmented with flutter control laws. In our approach, the controllers are designed based on a dynamical model, which is briefly discussed first. Details of the baseline control design, as well as the two different flutter suppression algorithms are discussed in the paper. Hardware-in-the-Loop testing of the controllers are reported before the first test flights of the aircraft.

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M3 - Conference Contribution (Conference Proceeding)

BT - Atmospheric Flight Mechanics Conference, AIAA SciTech Forum 2019

PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)

ER -

Flight control design for a highly flexible flutter demonstrator

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