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Manuel Pusch
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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
422018
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
302019
Structured control design for a highly flexible flutter demonstrator
M Pusch, D Ossmann, T Luspay
Aerospace 6 (3), 27, 2019
262019
Aeroelastic Mode Control using H2-optimal Blends for Inputs and Outputs
M Pusch
2018 AIAA guidance, navigation, and control conference, 0618, 2018
262018
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
242020
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
242019
-Optimal Blending of Inputs and Outputs for Modal Control
M Pusch, D Ossmann
IEEE Transactions on Control Systems Technology 28 (6), 2744-2751, 2019
202019
Integrated Optimization of Ailerons for Active Gust Load Alleviation
M Pusch, A Knoblach, T Kier
IFASD, 2015
182015
Integrated optimization of control surface layout for gust load alleviation
M Pusch, A Knoblach, T Kier
CEAS Aeronautical Journal 10, 1059-1069, 2019
142019
Blending of inputs and outputs for modal control of aeroelastic systems
M Pusch
Dr. Hut Verlag, 2020
122020
Fault tolerant control of an experimental flexible wing
D Ossmann, M Pusch
Aerospace 6 (7), 76, 2019
122019
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
122019
Design and optimization of an aeroservoelastic wind tunnel model
JKS Dillinger, YM Meddaikar, J Lübker, M Pusch, T Kier
Fluids 5 (1), 35, 2020
112020
Allocation of distributed flaps for gust load alleviation
M Pusch
2017 IEEE Conference on Control Technology and Applications (CCTA), 2120-2125, 2017
102017
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
82021
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
72021
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
72019
An integrated flexible aircraft model for optimization of lift distributions
TM Kier, M Leitner, Ö Süelözgen, M Pusch
AIAA Scitech 2019 Forum, 2039, 2019
72019
Advanced gust load alleviation using dynamic control allocation
M Pusch, TM Kier, M Tang, JK Dillinger, D Ossmann
AIAA SciTech 2022 Forum, 0439, 2022
52022
Aircraft Loads–A Wide Range of Disciplinary and Process-Related Issues in Simulation and Experiment
T Klimmek, RM Bogenfeld, E Breitbarth, J Dillinger, V Handojo, T Kier, ...
42020
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Artikelen 1–20