References
- Gilbert, T, and Trivailo, PM, 2001. Comparison of manoeuvre strains from non-linear co-rotational finite element model of an aircraft wing with flight test data. Presented at presented at the 9th Australian International Aerospace Congress.
- Dunn, SA, 1976. Technique for Unique Optimization of Dynamic Finite Element Models. New York: Academic Press; 1976.
- Levin, AJ, and Levin, RI, 1998. Dynamic finite element model updating using neural networks, Journal of Vibration and Sound 210 (5) (1998), pp. 593–607.
- Lee, U, 1995. Equivalent dynamic beam-rod models of aircraft wing structures, Aeronautical Journal 2088 (1995), pp. 450–457.
- Livne, E, and Navarro, I, 1999. Non-linear equivalent plate modelling of wing-box structures, Journal of Aircraft 36 (5) (1999), pp. 851–865.
- Kapania, RK, and Liu, Y, 2001. Equivalent skin analysis of wing structures using neural networks, AIAA Journal 39 (7) (2001), pp. 1390–1399.
- Haykin, SS, 1999. Neural Networks: A Comprehensive Foundation. New Jersey: Prentice Hall; 1999.
- Beale, M, and Demuth, H, 2001. Neural Network Toolbox User's Guide Version 4. Montana: The Maths Works Inc.; 2001.