[PDF][PDF] Blending of inputs and outputs for modal control of aeroelastic systems

M Pusch - 2020 - elib.dlr.de
The present thesis is the result of my work at the Institute of System Dynamics and Control at
the German Aerospace Center (DLR) in Oberpfaffenhofen, Germany. My thanks go to Prof …

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, 2021 - Springer
In this paper, the effect of nonlinear actuator dynamics on the performance of an active load
alleviation system for an experimental flexible wing is studied. Common nonlinearities such …

Advanced gust load alleviation using dynamic control allocation

M Pusch, TM Kier, M Tang, JK Dillinger… - AIAA SciTech 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-0439. vid Active control techniques
play a key role in today's aircraft developments to reduce structural loads during gust …

Performance analysis of control allocation using data‐driven integral quadratic constraints

M Pusch, D Ossmann, H Pfifer - Advanced Control for …, 2022 - Wiley Online Library
A new method is presented for evaluating the performance of a nonlinear control allocation
system within a linear control loop. To that end, a worst‐case gain analysis problem is …

[HTML][HTML] Characterization, Design Testing and Numerical Modeling of a Subsonic-Low Speed Wind Tunnel

A Lara, J Toledo, R Salazar - Ingeniería, 2022 - scielo.org.co
Method: Experimental measurements of the inlet velocity and pressure distribution of a wind
tunnel are performed. These empirical values are used as parameters to define boundary …

Das DLR-Projekt KonTeKst: Konzepte und Technologien für emissionsarme Kurzstreckenflugzeuge

WR Krüger, B Gerlinger, O Brodersen, T Klimmek… - 2020 - elib.dlr.de
Das Paper gibt eine Übersicht über die Arbeiten und Ergebnisse im Projekt KonTeKst. Im
Projekt wurden im ersten Hauptarbeitspaket zwei Flugzeugkonfigurationen mit einer …

Caracterización, pruebas de diseño y modelado numérico de un túnel de viento subsónico de baja velocidad

A Lara, J Toledo, RPS Romero - Ingeniería, 2022 - dialnet.unirioja.es
Método: Se efectúan mediciones experimentales del campo de velocidad y distribución
presión de entrada de un túnel de viento. Estos valores empíricos se usan como parámetros …