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International Journal of Aerospace Engineering
Volume 2013, Article ID 486020, 7 pages
http://dx.doi.org/10.1155/2013/486020
Research Article

A New Method for Initial Parameters Optimization of Guided Projectiles

The Academy of Equipment, Beijing 101416, China

Received 31 March 2013; Accepted 4 November 2013

Academic Editor: R. Ganguli

Copyright © 2013 Feng Bi-Ming and Nie Wan-Sheng. 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. P. Lu, D. B. Doman, and J. D. Schierman, “Adaptive terminal guidance for hypersonic impact in specified direction,” OMB 0704-0188.
  2. V. C. Lam, “Circular guidance laws with and without terminal velocity direction constraints,” in Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu, Hawaii, USA, August 2008. View at Publisher · View at Google Scholar · View at Scopus
  3. Y. Zhang, W. Zhang, J. Chen, and L. Shen, “Air-to-ground weapon delivery trajectory planning for UCAVs using gauss pseudospectral method,” Acta Aeronautica et Astronautica Sinica, vol. 32, no. 7, pp. 1240–1251, 2011. View at Publisher · View at Google Scholar · View at Scopus
  4. V. L. Siewert, J. C. Sussingham, and J. A. Farm, “6-DOF enhancement of precision guided munitions testing,” in Proceedings of the 36th AIAA Paper on Aerospace Sciences Meeting and Exhibit, Reno, Nev, USA, 1998. View at Publisher · View at Google Scholar
  5. H. Guo-Qiang, N. Ying, C. Fang et al., “Optimal release condition of no-power gliding bomb,” Flight Dynamics, vol. 27, no. 1, pp. 93–96, 2009. View at Google Scholar
  6. Z. Han-Yuan, Reentry Dynamics and Guidance. Changsha, Press of National University of Defense Technology, 1997.
  7. M.-S. Hou, “Optimal gliding guidance in vertical plane for standoff released guided bomb unit,” Acta Armamentarii, vol. 28, no. 5, pp. 572–575, 2007. View at Google Scholar · View at Scopus
  8. P. Williams, “Jacobi pseudospectral method for solving optimal control problems,” Journal of Guidance, Control, and Dynamics, vol. 27, no. 2, pp. 293–297, 2004. View at Google Scholar · View at Scopus
  9. T. R. Jorris, C. S. Schulz, F. R. Friedl, and A. V. Rao, “Constrained trajectory optimization using pseudospectral methods,” in Proceedings of the AIAA Atmospheric Flight Mechanics Conference and Exhibit, Honolulu, Hawaii, USA, August 2008. View at Publisher · View at Google Scholar · View at Scopus
  10. C. L. Darby and A. V. Rao, “An initial examination of using pseudospectral methods for timescale and differential geometric analysis of nonlinear optimal control problems,” in Proceedings of the AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Ontario, Canada, August 2008. View at Scopus
  11. E. R. Hartman and P. J. Johnston, “Mach 6 experimental and theoretical stability and performance of a cruciform missile at angle of attack up to 65°,” NASA Technical Paper 2733, 1987. View at Google Scholar