Publikationen

Silva, G. C., Silvestre, F. J., Donadon, M. V., Santos, O. S., Neto, A. B. G., Silva, R. G. A. d., Versiani, T. d. S. S., Gonzalez, P. J. and Bertolin, R. M. (2018). Active and Passive Control for Acceleration Reduction of an Aeroelastic Typical Wing Section. Journal of Vibration and Control, 2673-2687.

Silvestre, F. J., Guimarães Neto, A. B., Bertolin, R. M., da Silva, R. G. A. and Paglione, P. (2016). Aircraft control based on flexible aircraft dynamics. Journal of Aircraft. American Institute of Aeronautics and Astronautics, 262–271.

Silvestre, F. and Luckner, R. (2015). Experimental Validation of a Flight Simulation Model for Slightly Flexible Aircraft. AIAA Journal

Silvestre, F. J. (2013). Aeroservoelastic Investigation of a High-Aspect-Ratio Experimental Aircraft. Advances in Aerospace Guidance, Navigation and Control. Springer Verlag, 639-658.

Silvestre, F. J. (2012). Methodology for Modelling the Dynamics of Flexible, High-Aspect-Ratio Aircraft in the Time Domain for Aeroservoelastic Investigations. Dissertation, TU Berlin

Silvestre, F. J., Lamp, M., Meyer-Brügel, W. and Luckner, R. (2011). A Method for Aeroservoelastic Stability Analysis of an Optionally Piloted Aircraft. Proceedings of the IFASD International Forum on Aeroelasticity and Structural Dynamics, Paris

Silvestre, F. and Luckner, R. (2010). Methode zur flugmechanischen Simulation eines elastischen Flugzeugs bei Windstörungen im Zeitbereich. Deutscher Luft- und Raumfahrtkongress, Hamburg

Silvestre, F. and Luckner, R. (2009). Integrated model for the flight mechanics of a flexible aircraft in the time domain. IFASD 2009 International Forum on Aeroelasticity and Structural Dynamics, Seattle. IFASD.

Silvestre, F., Özkök, B., Luckner, R. and Weltin, U. (2009). A comparison study on modeling the airframe vibration of a motor glider during flight. CEAS 2009 European Air and Space Conference, Manchester. CEAS.

Silvestre, F. J. and Paglione, P. (2008). Dynamics and Control of a Flexible Aircraft. Proceedings of the AIAA Atmospheric Flight Mechanics Conference and Exhibit, Honolulu, Hawaii

Stukenborg, P. and Luckner, R. (2019). Evaluating the influence of continuous flap settings on the approach performance of an airliner using flight simulation. 67. Deutsche Luft- und Raumfahrtkongress

Stukenborg, P. and Luckner, R. (2018). Evaluating the influence of continuous flap settings on the take-off performance of an airliner using flight simulation. CEAS Aeronautical Journal, Vol. 9, No. 4. Springer Vienna, 671–681.

Stukenborg, P. and Luckner, R. (2017). Modellierung der aerodynamischen Beiwerte von stufenlos einstellbaren Hinterkantenklappen. DGLR Workshop Modellierung und Simulation in der Luftfahrt, Braunschweig

Stukenborg, P. and Luckner, R. (2017). Evaluating the Influence of Continuous Flap Settings on the Take-Off Performance of an Airliner Using Flight Simulation. 66. Deutsche Luft- und Raumfahrtkongress

Verri, A., Barros, J., Bussamra, F. L. S., Silvestre, F. J., Moreira, F. J. O., Guimaraes Neto, A. B., Cesnik, C. E. S. and Martins, J. S. (2018). Strain gages full bridge inside composite layers targeting wing shape feedback for flight control laws. 31st Congress of the International Council of the Aeronautical Sciences, ICAS

Versiani, T. d. S. S., Tsunematsu, D. Q., Donadon, M. V., Silvestre, F. J., Bernardo, A., Neto, G. and Guimarães, A. (2020). Aeroelastic behavior of a composite plate-like wing under piezoelectrically induced stresses. Mechanical Systems and Signal Processing, 106795.

Versiani, T. d. S. S., Silvestre, F. J., Neto, A. B. G., Rade, D. A., Silva, R. G. A. d., Donadon, M. V., Bertolin, R. M. and Silva, G. C. (2019). Gust load alleviation in a flexible smart idealized wing. Aerospace Science and Technology, 762 - 774.

Walde, G. (2018). Modellierungsrichtlinien für sicherheitskritische Software effizient anwenden. Ingenieurspiegel Luftfahrt: Fachmagazin für Ingenieure. Public Verlagsgesellschaft und Anzeigensagentur mbH, 22-24.

Walde, G., Lehmann, D. and Luckner, R. (2017). Verifying the Translation of a Flight Control Law Model from Simulink/Stateflow to Scade. 66. Deutsche Luft- und Raumfahrtkongress

Walde, G. and Luckner, R. (2016). Bridging the Tool Gap for Model-Based Design from Flight Control Function Design in Simulink to Software Design in SCADE. 2016 IEEE/AIAA 35th Digital Avionics Systems Conference (DASC), 1-10.

Walde, G. (2015). Übersetzbarkeit komplexer Flugsteuerungssoftware von Simulink/Stateflow nach SCADE. DGLR Workshop des Fachausschuss Q3.4 "Modellbasierte Softwareentwicklung in der Luft- und Raumfahrt - Was hat sich in der letzten Dekade getan?", München

Walde, G. and Luckner, R. (2015). Automatische Übersetzung komplexer Flugsteuerungssoftware von Simulink/Stateflow nach SCADE – Ein Erfahrungsbericht. 64. Deutschen Luft- und Raumfahrtkongress, Rostock

Walde, G. (2013). Entwicklung und Verifikation von GNC - Funktionen im Projekt LAPAZ. DGLR Workshop der Fachausschüsse Q3.4 & L6.3 "Durchgängige Entwicklung von GNC Funktionen - vom Algorithmus zur Embedded Software", München

Walde, G. and Hamann, A. (2012). ALEXIS – Friedliche Drohne für die Lehre. Luft- und Raumfahrt. AVIATIC.