Aeroservoelastic modeling and analysis of a highly flexible flutter demonstrator M Wuestenhagen, T Kier, YM Meddaikar, M Pusch, D Ossmann, ... 2018 atmospheric flight mechanics conference, 3150, 2018 | 45 | 2018 |
Structured control design for a highly flexible flutter demonstrator M Pusch, D Ossmann, T Luspay Aerospace 6 (3), 27, 2019 | 32 | 2019 |
Flight control design for a highly flexible flutter demonstrator T Luspay, D Ossmann, M Wuestenhagen, D Teubl, T Baár, M Pusch, ... AIAA Scitech 2019 Forum, 1817, 2019 | 32 | 2019 |
Aeroelastic Mode Control using H2-optimal Blends for Inputs and Outputs M Pusch 2018 AIAA guidance, navigation, and control conference, 0618, 2018 | 28 | 2018 |
Active flutter mitigation testing on the FLEXOP demonstrator aircraft B Takarics, B Patartics, T Luspay, B Vanek, C Roessler, J Bartasevicius, ... AIAA Scitech 2020 Forum, 1970, 2020 | 25 | 2020 |
Aeroelastic modeling and control of an experimental flexible wing M Pusch, D Ossmann, J Dillinger, TM Kier, M Tang, J Lübker AIAA scitech 2019 forum, 0131, 2019 | 25 | 2019 |
-Optimal Blending of Inputs and Outputs for Modal Control M Pusch, D Ossmann IEEE Transactions on Control Systems Technology 28 (6), 2744-2751, 2019 | 20 | 2019 |
Integrated Optimization of Ailerons for Active Gust Load Alleviation M Pusch, A Knoblach, T Kier IFASD, 2015 | 18 | 2015 |
Integrated optimization of control surface layout for gust load alleviation M Pusch, A Knoblach, T Kier CEAS Aeronautical Journal 10, 1059-1069, 2019 | 15 | 2019 |
Blending of inputs and outputs for modal control of aeroelastic systems M Pusch Dr. Hut Verlag, 2020 | 14 | 2020 |
Design and wind tunnel test of an actively controlled flexible wing WR Krüger, J Dillinger, MY Meddaikar, J Lübker, M Tang, T Meier, ... International Forum on Aeroelasticity and Structural Dynamics 2019, IFASD 2019, 2019 | 14 | 2019 |
Design and optimization of an aeroservoelastic wind tunnel model JKS Dillinger, YM Meddaikar, J Lübker, M Pusch, T Kier Fluids 5 (1), 35, 2020 | 13 | 2020 |
Fault tolerant control of an experimental flexible wing D Ossmann, M Pusch Aerospace 6 (7), 76, 2019 | 13 | 2019 |
Allocation of distributed flaps for gust load alleviation M Pusch 2017 IEEE Conference on Control Technology and Applications (CCTA), 2120-2125, 2017 | 10 | 2017 |
Identification and assessment of a nonlinear dynamic actuator model for controlling an experimental flexible wing M Tang, M Böswald, Y Govers, M Pusch CEAS Aeronautical Journal 12, 413-426, 2021 | 9 | 2021 |
Identification and assessment of a nonlinear dynamic actuator model for gust load alleviation in a wind tunnel experiment M Tang, M Böswald, Y Govers, M Pusch CEAS Aeronautical Journal, 2021 | 7 | 2021 |
Blending of inputs and outputs for modal velocity feedback M Pusch, D Ossmann 2019 27th Mediterranean Conference on Control and Automation (MED), 530-535, 2019 | 7 | 2019 |
An integrated flexible aircraft model for optimization of lift distributions TM Kier, M Leitner, Ö Süelözgen, M Pusch AIAA Scitech 2019 Forum, 2039, 2019 | 7 | 2019 |
Sink or swim: A tutorial on the control of floating wind turbines D Stockhouse, M Phadnis, A Henry, N Abbas, M Sinner, M Pusch, LY Pao 2023 American Control Conference (ACC), 2512-2529, 2023 | 5 | 2023 |
Advanced gust load alleviation using dynamic control allocation M Pusch, TM Kier, M Tang, JK Dillinger, D Ossmann AIAA SciTech 2022 Forum, 0439, 2022 | 5 | 2022 |