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Conference Papers & Publications

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The list below collects publications produced by PACE staff for scientific and commercial forums, results from collaborations with universities or studies involving the application of one of our products.

2017

Sizing, Integration and Performance Evaluation of Hybrid Electric Propulsion Subsystem Architectures.

Cinar, G., Mavris, D.N., Emeneth, M., Schneegans, A., Riediger, C., Fefermann, Y., Isikveren, A. (2017)
55th AIAA Aerospace Sciences Meeting (AIAA SciTech Forum)
January 9-13, 2017, Grapevine (TX), USA

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Development of Parametric Power Generation and Distribution Subsystem Models at Conceptual Aircraft Design Stage.

Cinar, G., Mavris, D.N., Emeneth, M., Schneegans, A., Fefermann, Y. (2017)
55th AIAA Aerospace Sciences Meeting (AIAA SciTech Forum)
January 9-13, 2017, Grapevine (TX), USA

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2016

A Methodology for Sizing and Analysis of Electric Propulsion Subsystems for Unmanned Aerial Vehicles.

Cinar, G., Emeneth, M., and Mavris, D.N. (2016)
54th AIAA Aerospace Sciences Meeting (AIAA SciTech)
January 4-8, 2016, San Diego (CA), USA

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2015

An integrated approach to vehicle and subsystem sizing and analysis for novel subsystem architectures.

Chakraborty, I., Mavris, D.N., Emeneth, M., and Schneegans, A. (2015)
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.
Published online July 20, 2015, DOI: 10.1177/0954410015594399

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2014

A Methodology for Vehicle and Mission Level Comparison of More Electric Aircraft Subsystem Solutions – Application to the Flight Control Actuation System.

Chakraborty, I., Mavris, D.N., Emeneth, M., and Schneegans, A. (2014)
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.
Published online July 28, 2014, DOI: 10.1177/0954410014544303

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2015 AIAA Best Paper:

A Requirements-driven Methodology for Integrating Subsystem Architecture Sizing and Analysis into the Conceptual Aircraft Design Phase.

Chakraborty, I., Trawick, D., Mavris, D.N., Emeneth, M., and Schneegans, A. (2014)
14th AIAA Aviation Technology, Integration, and Operations Conference
June  16-20, 2014, Atlanta (GA), USA

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PACE's Mathias Ementh and Imon Chakraborty (ASDL) holding the AIAA 2015 Best Paper Award certificate.
AIAA 2015 Best Paper Award – Left to right: Mathias Emeneth (PACE), Imon Chakraborty and Prof. Dimitri N. Mavris (ASDL)

Aircraft Conceptual Design: Tools Evaluation.

Locatelli, D., Riggins, B., Schetz, J.A., Kapania, R.K., Robic, B., Leenaert, B., and Poquet, T. (2014)
14th AIAA Aviation Technology, Integration, and Operations Conference
June 16-20, 2014, Atlanta (FL), USA

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A System and Mission Level Analysis of Electrically Actuated Flight Control Surfaces using Pacelab SysArc.

Chakraborty, I., Mavris, D.N., Emeneth, M., and Schneegans, A. (2014)
AIAA Science and Technology Forum and Exposition (SciTech)
Jan 13-17, 2014, National Harbor (MD), USA

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2013

Robust Aircraft Subsystem Conceptual Architecting.

Jackson, D.W. (2013)
Ph.D. Georgia Institute of Technology

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2012

Optimisation Robuste des Aéronefs et des Groups Turboréacteurs.

Couturier, P. (2012)
M.Sc. École polytechnique de Montréal

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Parametric Control Surface Modeling During Early Design Stages in Pacelab Suite.

Emeneth, M., Garmendia, D., Mavris, D. (2012).
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
January 09-12, 2012, Nashville (TN), USA

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Advanced Methods for Propulsion System Integration in Aircraft Conceptual Design.

Seitz, A. (2012)
Ph.D. University of Munich

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Investigating Systems Architectures at the Aircraft Level – Towards a Holistic Framework for the Aircraft Systems Design Process.

Schneegans, A. (2012)
Deutscher Luft- und Raumfahrtkongress
September 10-12, 2012, Berlin, Germany.

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2011 and earlier

Knowledge-Based Preliminary Design of Aero-Engine Gas-Generators.

Bretschneider, S. (2011)
Ph.D. University of Stuttgart

Systems Architecture Design – A Software Development for the JTI Clean Sky Green Regional Aircraft Program.

Schneegans, A. (2011)
11th AIAA Aviation Technology, Integration, and Operations Conference
September 20-22, 2011, Virginia Beach (VA), USA

The All-Electric Regional Aircraft – A New Design Methodology for Vehicle-Level Systems Architecture Design.

Schneegans, A. (2011)
58th Canadian Aeronautics and Space Institute (CASI) Aeronautics Conference - AERO 2011
April 26-28, 2011, Montreal (QC), Canada

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A Modeling Methodology and Environment for Integrated Trim Analysis for a Reusable Booster System.

Robertson, B., Crowley, D., Garmendia, D., Douglass, R., Mavris, D., and Hellman, B. (2011)
49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
January 4-7, 2011, Orlando (FL), USA

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Integrierte Produkt- und Prozessmodellierung. Unterstützung der Systementwicklung für eine Avionik-Plattform (Integrated product and process modelling. Support of system development for avionics).

Girod, M., Schramm, A., Schultz, R., Wintrich, N. (2011)
Zeitschrift für wirtschaftlichen Fabrikbetrieb. ZWF 106 (6). pp.454-457

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Comparison of Powered-Lift Turbofan Aircraft with Conventional Turboprop Aircraft for ESTOL Application.

Gologan, C., Schmitt, D. (2010)
27th International Congress of Aeronautical Sciences
September 19-24, 2010, Nice, France

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New Design Methodology for the Development and Optimization of Payload and System Architectures for Unmanned Aircraft Systems.

Ehlermann, F. (2010)
4th International Conference UAV World
November 3-4, 2010, Frankfurt/Main, Germany

Formulation and Implementation of a Methodology for Aircraft Subsystem Architecture Selection.

Zaidi, T. (2009)
TEOS III Forum at the 13th European Conference on Power Electronics and Applications
September 8-10, 2009, Barcelona, Spain

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Applying KBE Technologies to the Early Phases of Multidisciplinary Product Design.

Schneegans, A. and Ehlermann, F. (2007)
In: Frank-Lothar Krause, ed. 2007. The Future of Product Development. Proceedings of the 17th CIRP Design Conference. Berlin: Springer. pp. 587-596

Preface and table of contents