Optimal design of unmanned aerial vehicles using parametric CAX systems

2011;
: pp. 35 – 37
Authors: 

Lukaszewicz A.

Bialystok University of Technology, Faculty of Mechanical Engineering

The article is devoted to solution of the optimal design tasks of Unmanned Aerial Vehicles at different stages. The tasks for all UAV’s design stages are considered and CAx tools for optimal design are proposed based on empirical experience.

1. Łukaszewicz A. (2009): Geometrical modelling of UAV using parametric CAx systems, In: the European Micro Air Vehicle Conference and Competition 2009, TU Delft, the Netherlands, electronic version (www.emav2009.org/EMAV-final-papers/paper_61.pdf); 2. Fishburn P.C. (1970): Utility Theory for Decision Making, J. Wiley and Sons, New York; 3.Vincke Ph. (1992): Multicriteria Decision Aid, J. Wiley and Sons; 4. Doumpos M., Zapounidis C. (2002): Multicriteria Decision Aid Classification Methods, Kluwer Academic Publishers, Dordrecht; 5. Stinton, D. (1985): The Design of the Aeroplane, Collins Professional and Technical Books; 6. Raymer D. (1999): Aircraft Design: A Conceptual Approach, AIAA Education Series, Reston, VA; 7. Brusow W: (1996): Optymalne projektowanie wielozadaniowych statków latających, Biblioteka Naukowa Instytutu Lotnictwa, Warszawa; 8. Keane A.J., Nair P.B. (2004): Computational Approaches for Aerospace Design, First Edition, Wiley; 9. Sobester A., Keane A.J., Scanlan J., Bresslo N.W., (2005): Conceptual Design of UAV Air-frames Using a Generic Geometry Service, AIAA Infotech@Aerospace, Arlington, VA, (Retrieved: March 2, 2010 from: http://www.soton.ac.uk/~as7/publ/infotech05.pdf); 10. Sobester A., Keane A.J. (2006): Supervised Learning Approach to Computer-Aided Design Ge-ometry Repair, AIAA Journal, Vol. 44, No. 2, pp. 282– 289; 11. Sobester A., Keane A.J. (2006): Multidisciplinary Design Optimization of UAV Airframes, 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Confer-ence, AIAA 2006- 1612; 12. La Rocca G., Krakers L., van Tooren M.J.L. (2002): Development of an ICAD Generative Model for Blended Wing Body Aircraft Design, 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimisation, Atlanta; 13. Osterheld C., Heinze W., Horst P. (2001): Preliminary Design of a Blended Wing Body Configuration using the Design Tool PrADO, CEAS Conference on Multidisciplinary Aircraft Design and Optimisation, Koln; 14. Liu H., Wang G.L., Lu X.L., Wu Z. (2004): Preliminary Investigation of Integrated Multidisciplinary Optimization in Aircraft Conceptual Design, 10th AIAA/ISSMO Multidiscipli-nary Analysis and Optimization Conference, Albany; 15. Antoine N., Kroo I., Willcox K., Barter G. (2004): A Framework for Aircraft Conceptual Design and Environmental Performance Studies, 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany; 16. Perez R.E., Liu H.H.T., Behdinan K. (2004): Evaluation of Multidisciplinary Optimization Ap-proaches for Aircraft Conceptual Design, 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany; 17. Romeo G., Frulla G., Cestino E. (2007): Design of a High-Altitude Long-Endurance Solar-Powered Unmanned Air Vehicle for Multi-Payload and Operations, Proc. IMechE Part G: J. Aerospace Engineering, Vol. 221, 199–216;