Table of Contents Author Guidelines Submit a Manuscript
Mathematical Problems in Engineering
Volume 2017, Article ID 1409829, 8 pages
https://doi.org/10.1155/2017/1409829
Research Article

Optimization Plug Mode of External Fuel and Weapons for Less Changing Aircraft Center of Gravity

School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

Correspondence should be addressed to Mingxu Yi; moc.361@88uxgnimiy

Received 13 January 2017; Revised 14 March 2017; Accepted 20 April 2017; Published 18 June 2017

Academic Editor: Ilhan Tuzcu

Copyright © 2017 Zeyang Zhou et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Linked References

  1. C. Han, L. Yang, and J. Zhang, “Adaptive nonsingular fast terminal sliding mode control for aircraft with center of gravity variations,” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 229, no. 1, pp. 4–9, 2015. View at Publisher · View at Google Scholar · View at Scopus
  2. X. Yang, M. Luo, J. Zhang, and L. Yang, “Aircraft centre-of-gravity estimation using Gaussian process regression models,” in Proceedings of the IEEE International Conference on Aircraft Utility Systems (AUS '16), pp. 991–995, IEEE, Beijing, China, October 2016. View at Publisher · View at Google Scholar
  3. Aircraft weight and center of gravity indicator system, U.S. Patent 3,701,279. 1972-10-31.
  4. A. Gupta, C. Moreno, H. Pfifer, B. Taylor, and G. J. Balas, “Updating a finite element based structural model of a small flexible aircraft,” in Proceedings of the AIAA Science and Technology Forum. View at Publisher · View at Google Scholar
  5. Y. Z. Li, C. S. Yuan, and L. Zhang, “Analyze the C.G of a UAV based on load task,” Science Technology and Engineering, vol. 11, no. 15, pp. 3472–3475, 2011. View at Google Scholar
  6. H. Li, J. Zhang, and J. Yan, “Effects of partial fuel pump failure on center of gravity control for high-speed aircraft,” in Proceedings of the International Conference on Aircraft Utility Systems (AUS), pp. 146–150, IEEE, 2016.
  7. H. Li, J. Zhang, and J. Yan, “Analysis of the influence of partial fuel transfer line leak on active center of gravity control,” in Proceedings of the International Conference on Aircraft Utility Systems (AUS), pp. 151–155, IEEE, Beijing, China, October 2016. View at Publisher · View at Google Scholar
  8. A. Jungo, F. P. Gallaire, and J. Vos, Development of the CEASIOM aircraft design environment for novel aircraft configurations [D]. [Master, thesis], Ecole polytechnique federale de Lausanne, 2014.
  9. P. Mardanpour, D. H. Hodges, R. Neuhart, and N. Graybeal, “Engine placement effect on nonlinear trim and stability of flying wing aircraft,” Journal of Aircraft, vol. 50, no. 6, pp. 1716–1725, 2013. View at Publisher · View at Google Scholar · View at Scopus
  10. Q. C. Zhen, “Probe into the C.G. position of minimum drag for J-7 aircraft,” Flight Dynamics, vol. 3, pp. 40–46, 1991. View at Google Scholar
  11. G. Sachs, “Minimum trimmed drag and optimum c.g. position,” Journal of Aircraft, vol. 15, no. 8, pp. 456–459, 1978. View at Publisher · View at Google Scholar · View at Scopus
  12. W. J. Xu and Z. M. Liu, “Effect of center-of-gravity position on aircraft drag and flight performance,” Flight Dynamics, vol. 17, no. 1, pp. 54–58, 1999. View at Google Scholar
  13. G. Wang, Y. Hu, and B. Song, “Tailless UAV design optimization under center of gravity location uncertainty,” Acta Aeronautica et Astronautica Sinica, vol. 36, no. 7, pp. 2214–2224, 2015. View at Publisher · View at Google Scholar · View at Scopus
  14. J. H. Diekmann, “Trim analysis of nonlinear flight dynamics for a civil aircraft with active high-lift system,” in Deutscher Luft- und Raumfahrtkongress, Stuttgart, Deutschland, September 2013.
  15. J. Y. Tang, C. Z. Wang, B. Wang, and etal., “Methods of calculating and analysis of aircraft's gravity position,” Aeronautical Computing Technique, vol. 46, no. 3, pp. 72–74, 2016. View at Google Scholar
  16. B. D. Dancila, R. Botez, and D. Labour, “Fuel burn prediction algorithm for cruise, constant speed and level flight segments,” Aeronautical Journal, vol. 117, no. 1191, pp. 491–504, 2013. View at Publisher · View at Google Scholar · View at Scopus
  17. R. F. Patron, R. Botez, and D. Labour, “Low calculation time interpolation method on the altitude optimization algorithm for the FMS CMA-9000 improvement on the A310 and L-1011 aircraft,” in Proceedings of Aviation Technology, Integration and Operation (ATIO) Conference and International Powered Lift Conference (IPLC), Los Angeles, CA, USA. View at Publisher · View at Google Scholar
  18. C. Ivester, J. Mckee, W. Johnson et al., Compact aircraft galley and lavatory arrangement and articulating lavatory partition for an aircraft, U.S. Patent Application 14/175,537. 2014:2-7.
  19. X. L. Jia, L. J. Huang, Z. M. Zhang, and et al., “Development and Application of CAPP system for aircraft airborne weapon gallows product,” Aviation Precision Manufacturing Technology, vol. 44, no. 2, pp. 52–55, 2008. View at Google Scholar
  20. L. Xia, “Analysis the effect of carrying and launching weapon on the stability and motion parameter of helicopter,” Flight Dynamics, no. 3, pp. 33–41, 1990. View at Google Scholar
  21. M. Zhang, L. Wang, D. Ren, and et al., “Design and realization of weapon store simulator,” Trainer, no. 4, pp. 46–49, 2013. View at Google Scholar
  22. W. L. Feng, J. L. Cheng, and L. Y. Lv, “Safety analysis method in weapons store delivery,” Journal of Projectiles, Rockets, Missiles and Guidance, vol. 34, no. 4, pp. 191–195, 2014. View at Google Scholar
  23. Z. Q. Luo, “1553B bus error correction technology in the management system of aircraft weapon,” Electronics Optics & Control, vol. 3, 1987. View at Google Scholar