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Analysis of the Effects of Modeling Depth and Parameter Uncertainties on the System Behavior of a Multifunctional High Lift Actuation System
Technical Paper
2018-01-1918
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
Modeling and simulation have become an important aspect of the design and development process of aircraft systems. During the design of high lift actuation systems for example, the dynamic loads in the transmission are estimated by simulation. Nevertheless huge development efforts and financial resources are still invested in physical testing. These integration and testing phases take place at a late stage in the design process. Therefore, identified malfunctions and development errors lead to undesired iterations and thus to high costs as well as to an increased development time. This issue is emphasized as system complexity is rises continuously in conjunction with an increase in the number of interconnections and functionality. Hence, early and continuous virtual testing activities on the overall system level become increasingly important. In order to establish such a process, this paper analyzes the effects of modeling depth and parameter uncertainties on the overall system behavior considering nominal operation as well as failure cases. It identifies which test cases can be performed in which development phase depending on the information required. The modeling and simulation is implemented in the multiphysics and object-oriented simulation environment Matlab/Simulink/Simscape using an example of a multifunctional high lift actuation system.
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Citation
Schäfer, A. and Schmid, M., "Analysis of the Effects of Modeling Depth and Parameter Uncertainties on the System Behavior of a Multifunctional High Lift Actuation System," SAE Technical Paper 2018-01-1918, 2018, https://doi.org/10.4271/2018-01-1918.Also In
References
- Ulmer , T. and Amin , J. Virtual Testing of High Lift Systems SAE Technical Paper 2013-01-2280 2013 10.4271/2013-01-2280
- Jandaurek , K. and Johst , M. Development Trends and Innovations in Aerospace System Testing Using the Example of High-Lift Proceedings of the 55th AIAA Aerospace Sciences Meeting 2007 10.2514/6.2017-0548
- Junghanns , A. , Mauss , J. , and Tatar , M. Tatar: TestWeaver - A Tool for Simulation-Based Test of Mechatronic Designs the 6th International Modelica Conference Germany Mar. 3-4 2008
- Cappuzzo , F. , Broca , O. , and Allain , L. Methodologies and Processes to Achieve Earlier Virtual Integration of Aircraft Systems the 6th European Conference for Aerospace Sciences Poland June 29-July 3 2015
- Hans , C. and Hribernik , K. NFF Special Session - Potentials of Applying Methods, Tools, Processes and Knowledge from Testing in Product Development to the NFF Problem Proceedings of the 10th CIRP Conference on Industrial Product-Service Systems 2014 53 58 10.1016/j.procir.2014.07.131
- Goulain , M. Overview of Clean Sky 2 Programme the AirTN-NextGen Workshop on Virtual Testing, Towards Virtual Certification 2016
- Kroll , N. , Abu-Zurayk , M. , Dimitrov , D. , Franz , T. et al. DLR Project Digital-X: Towards Virtual Aircraft Design and Flight Testing Based on High-Fidelity Methods CEAS Aeronautical Journal 7 3 2016 10.1007/s13272
- Reckzeh , D. Multifunctional Wing Moveables Design of the A350XWB and the Way to Future Concepts Proceedings of the 29th Congress of the International Council of the Aeronautical Sciences Russia Sept. 7-24 2017
- Strüber , H. The Aerodynamic Design of the A350 XWB-900 High Lift System Proceedings of the 29th Congress of the International Council of the Aeronautical Sciences Russia Sept. 7-24 2017
- Vechtel , D. , Hauber , B. , and Looye , G. Analysis of a Multi-Functional High-Lift System Driven by an Active Differential Gear Box CEAS Aeronautical Journal 5 227 2014 10.1007/s13272-014-0102-7
- Recksiek , M. Hochauftriebssysteme - von der Flugzeugkonfiguration zur Systementwicklung the Hamburg University of Applied Sciences 2004
- Kreitz , T. , Johnsen , S. , and Thielecke , F. Virtuelles Testen Elektro-Mechanische Aktuatoren im Rahmen Eines Modellbasierten Entwurfsprozesses the Deutscher Luft- und Raumfahrtkongress Germany Sept. 10-12 2013
- Kreitz , T. and Thielecke , F. Virtual Integration of an All-Electric Flight Control System Architecture and the Aircraft Electrical Power Distribution Network SAE Technical Paper 2016-01-2034 2016 10.4271/2016-01-2034
- Verein Deutscher Ingenieure 2004
- Pfennig , M. 2012
- Arriola , D. and Thielecke , F. Model-Based Design and Experimental Verification of a Monitoring Concept for an Active-Active Electromechanical Aileron Actuation System Mechanical Systems and Signal Processing 94 322 345 2017 10.1016/j.ymssp.2017.02.039
- Karam , W. and Mare , J.-C. Modelling and Simulation of Mechanical Transmission in Roller-Screw Electromechanical Actuators Aircraft Engineering and Aerospace Technology 81 4 288 298 2009 10.1108/00022660910967273
- Kreitz , T. , Arriola , D. , and Thielecke , F. Virtual Performance Evaluation for Electromechanical Actuators Considering Parameter Uncertainties the Recent Advances in Aerospace Actuation Systems and Components France Apr. 2-3 2014
- Roy , C. and Oberkampf , W. A Comprehensive Framework for Verification, Validation, and Uncertainty Quantification in Scientific Computing Computer Methods in Applied Mechanics and Engineering 200 25-28 2131 2144 2011 10.1016/j.cma.2011.03.016
- Helton , J.C. , Johnson , J.D. , Sallaberry , C.J. , and Storlie , C.B. Survey of Sampling-Based Methods for Uncertainty and Sensitivity Analysis Reliability Engineering & System Safety 91 2006 1175 1209 2006 10.1016/j.ress.2005.11.017
- Borgonovo , E. Sensitivity Analysis Springer International Publishing 2017 10.1007/978-3-319-52259-3
- Saltelli , A. , Tarantola , S. , and Chan , K.P.-S. A Quantitative Model-Independent Method for Global Sensitivity Analysis of Model Output Technometrics 41 1 39 56 1999 10.1080/00401706.1999.10485594
- Siebertz , K. , van Bebber , D. , and Hochkirchen , T. Statistische Versuchsplanung: Design of Experiments Springer Vieweg 2017 10.1007/978-3-662-55743-3
- Sobol , I.M. Sensitivity Estimates for Nonlinear Mathematical Models Mathematical Modeling & Computational Experiment 1 407 414 1993
- Murray-Smith , D.J. Modelling and Simulation of Integrated Systems in Engineering Woodhead Publishing 2012 978-0-85709-078-2
- Oberkampf , W.L. and Roy , C.J. Verification and Validation in Scientific Computing Cambridge University Press 2010 10.1017/CBO9780511760396
- Oden , T. , Moser , R. , and Ghattas , O. SIAM News 43 49 2010
- Helton , J.C. and Davis , F.J. Latin Hypercube Sampling and the Propagation of Uncertainty in Analyses of Complex Systems Reliability Engineering & System Safety 81 1 23 69 2003 10.1016/S0951-8320(03)00058-9
- McKay , M.D. , Beckman , R.J. , and Conover , W.J. Comparison of Three Methods for Selecting Values of Input Variables in the Analysis of Output from a Computer Code Technometrics 21 2 239 245 1979 10.1080/00401706.1979.10489755
- Stein , M. Large Sample Properties of Simulations Using Latin Hypercube Sampling Technometrics 29 2 143 151 1987 10.1080/00401706.1987.10488205
- Park , J.-S. Optimal Latin-Hypercube Designs for Computer Experiments Journal of Statistical Planning and Inference 39 1 95 111 1994 10.1016/0378-3758(94)90115-5
- Isermann , R. Mechatronic Systems London Springer-Verlag 2005 10.1007/1-84628-259-4
- Benischke , S. and Thielecke , F. Evaluation of Control Strategies for Single Flap Drive Systems in Multifunctional High Lift Systems SAE Technical Paper 2015-01-2479 2015 10.4271/2015-01-2479
- Olsson , H. , Aström , K.J. , Candus de Wit , C. , Gäfvert , M. et al. Friction Models and Friction Compensation European Journal of Control 4 176 195 1998 10.1016/S0947-3580(98)70113-X
- Armstrong-Hélouvry , B. Control of Machines with Friction US Springer 1991 10.1007/978-1-4615-3972-8
- Mare , J.-C. Friction Modelling and Simulation at System Level: Considerations to Load and Temperature Effects Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering 229 221 2014 10.1177/0959651814548440
- Braiwish , N. 2016
- Fitzgerald , A.E. , Kingsley , C. , and Umans , S.D. Electric Machinery McGraw-Hill 2003 0-07-366009-4
- Schröder , D. Elektrische Antriebe - Grundlagen Berlin/Heidelberg Springer 2007 10.1007/978-3-540-73005-7
- Liepmann , D. and Stephanopoulos , G. Development and Global Sensitivity Analysis of a Closed Ecosystem Model Ecological Modelling 30 1985 13 47 1985 10.1016/0304-3800(85)90035-3
- Maschke , G. 1988
- Budinger , M. , Liscouet , J. , Hospital , F. , and Mare , J.-C. Estimation Models for the Preliminary Design of Electromechanical Actuators Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 226 3 2011 10.1177/0954410011408941
- Bierig , A. , Nikodem , F. , Gallun , P. , and Greiner-Perth , C. Design of the General Systems for the SAGITTA Demonstrator UAV Proceedings of the International Conference on Unmanned Aircraft Systems 2017 10.1109/ICUAS.2017.7991305
- Borello , L. and Villero , G. Mechanical Failures of Flap Control Systems and Related Monitoring Techniques the 21th Congress of International Council of the Aeronautical Sciences Australia Sept. 13-18 1998