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International Journal of Aerospace Engineering
Volume 2018, Article ID 3968242, 10 pages
https://doi.org/10.1155/2018/3968242
Research Article

New Integrated Guidance and Control of Homing Missiles with an Impact Angle against a Ground Target

1Institute of Precision Guidance and Control, Northwestern Polytechnical University, Shaanxi 710072, China
2Beijing Aerospace Technology Institute, Beijing 100074, China

Correspondence should be addressed to Jianguo Guo; nc.ude.upwn@ougnaijoug

Received 4 February 2018; Revised 25 May 2018; Accepted 9 July 2018; Published 5 August 2018

Academic Editor: Giovanni Palmerini

Copyright © 2018 Shengjiang Yang 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. M. Levy, T. Shima, and S. Gutman, “Linear quadratic integrated versus separated autopilot-guidance design,” Journal of Guidance, Control, and Dynamics, vol. 36, no. 6, pp. 1722–1730, 2013. View at Publisher · View at Google Scholar · View at Scopus
  2. P. K. Menon and E. J. Ohlmeyer, “Integrated design of agile missile guidance and autopilot systems,” Control Engineering Practice, vol. 9, no. 10, pp. 1095–1106, 2001. View at Publisher · View at Google Scholar · View at Scopus
  3. N. F. Palumbo, B. E. Reardon, and R. A. Blauwkamp, “Integrated guidance and control for homing missiles,” Johns Hopkins APL Technical Digest, vol. 25, no. 2, pp. 121–139, 2004. View at Google Scholar
  4. M. Z. Hou, X. L. Liang, and G. R. Duan, “Adaptive block dynamic surface control for integrated missile guidance and autopilot,” Chinese Journal of Aeronautics, vol. 26, no. 3, pp. 741–750, 2013. View at Publisher · View at Google Scholar · View at Scopus
  5. D. E. Williams, J. Richman, and B. Friedland, “Design of an integrated strapdown guidance and control system for a tactical missile,” in Guidance and Control Conference, pp. 57–66, Gatlinburg, TN, USA, August 1983. View at Publisher · View at Google Scholar
  6. T. Shima, M. Idan, and O. M. Golan, “Sliding mode control for integrated missile autopilot-guidance,” in AIAA Guidance, Navigation, and Control Conference and Exhibit, Providence, Rhode Island, August 2004.
  7. D. Chwa, J. Y. Choi, and S. G. Anavatti, “Observer-based adaptive guidance law considering target uncertainties and control loop dynamics,” IEEE Transactions on Control Systems Technology, vol. 14, no. 1, pp. 112–123, 2006. View at Publisher · View at Google Scholar · View at Scopus
  8. M. Xin, S. N. Balakrishnan, and E. J. Ohlmeyer, “Integrated guidance and control of missiles with θ-D method,” IEEE Transactions on Control Systems Technology, vol. 14, no. 6, pp. 981–992, 2006. View at Publisher · View at Google Scholar · View at Scopus
  9. R. Padhi and C. Chawla, “Neuro-adaptive augmented dynamic inversion based PIGC design for reactive obstacle avoidance of UAVs,” in AIAA Guidance, Navigation, and Control Conference, Portland, Oregon, August 2011. View at Publisher · View at Google Scholar
  10. X. Wang and J. Wang, “Partial integrated guidance and control for missiles with three-dimensional impact angle constraints,” Journal of Guidance, Control, and Dynamics, vol. 37, no. 2, pp. 644–657, 2014. View at Publisher · View at Google Scholar · View at Scopus
  11. X. Wang and J. Wang, “Partial integrated guidance and control with impact angle constraints,” Journal of Guidance, Control, and Dynamics, vol. 38, no. 5, pp. 925–936, 2015. View at Publisher · View at Google Scholar · View at Scopus
  12. F. B. Ibarrondo and P. Sanz-Aránguez, “Integrated versus two-loop guidance-autopilot for a dual control missile with high-order aerodynamic model,” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 230, no. 1, pp. 60–76, 2016. View at Publisher · View at Google Scholar · View at Scopus
  13. X. Liu, W. Huang, and L. du, “An integrated guidance and control approach in three-dimensional space for hypersonic missile constrained by impact angles,” ISA Transactions, vol. 66, pp. 164–175, 2017. View at Publisher · View at Google Scholar · View at Scopus
  14. H. Yan, S. P. Tan, and Y. Z. He, “A small-gain method for integrated guidance and control in terminal phase of reentry,” Acta Astronautica, vol. 132, pp. 282–292, 2017. View at Publisher · View at Google Scholar · View at Scopus
  15. H. Yan, X. Wang, B. Yu, and H. Ji, “Adaptive integrated guidance and control based on backstepping and input-to-state stability,” Asian Journal of Control, vol. 16, no. 2, pp. 602–608, 2014. View at Publisher · View at Google Scholar · View at Scopus
  16. S. Wang, W. H. Wang, and S. F. Xiong, “Impact angle constrained three-dimensional integrated guidance and control for STT missile in the presence of input saturation,” ISA Transactions, vol. 64, pp. 151–160, 2016. View at Publisher · View at Google Scholar · View at Scopus
  17. H. Song and T. Zhang, “Fast robust integrated guidance and control design of interceptors,” IEEE Transactions on Control Systems Technology, vol. 24, no. 1, pp. 349–356, 2016. View at Publisher · View at Google Scholar · View at Scopus
  18. Z. Cong and W. Yun-jie, “Non-singular terminal dynamic surface control based integrated guidance and control design and simulation,” ISA Transactions, vol. 63, pp. 112–120, 2016. View at Publisher · View at Google Scholar · View at Scopus
  19. S. He, T. Song, and D. Lin, “Impact angle constrained integrated guidance and control for maneuvering target interception,” Journal of Guidance, Control, and Dynamics, vol. 40, no. 10, pp. 2653–2661, 2017. View at Publisher · View at Google Scholar · View at Scopus
  20. S. M. He, J. Wang, and W. Wang, “A novel sliding mode guidance law without line-of-sight angular rate information accounting for autopilot lag,” International Journal of Systems Science, vol. 48, no. 16, pp. 3363–3373, 2017. View at Publisher · View at Google Scholar · View at Scopus
  21. J. G. Guo, Y. Xiong, and J. Zhou, “A new sliding mode control design for integrated missile guidance and control system,” Aerospace Science and Technology, vol. 78, pp. 54–61, 2018. View at Publisher · View at Google Scholar · View at Scopus
  22. H. Mingzhe and D. Guangren, “Integrated guidance and control of homing missiles against ground fixed targets,” Chinese Journal of Aeronautics, vol. 21, no. 2, pp. 162–168, 2008. View at Publisher · View at Google Scholar · View at Scopus
  23. X. F. Qian, R. X. Lin, and Y. N. Zhao, Missile Flight Mechanics, Beijing Institute of Technology Press, Beijing, 2000.
  24. D. Ginoya, P. D. Shendge, and S. B. Phadke, “Sliding mode control for mismatched uncertain systems using an extended disturbance observer,” IEEE Transactions on Industrial Electronics, vol. 61, no. 4, pp. 1983–1992, 2014. View at Publisher · View at Google Scholar · View at Scopus
  25. D. Zhou, C. D. Mu, and W. L. Xu, “Adaptive sliding-mode guidance of a homing missile,” Journal of Guidance, Control, and Dynamics, vol. 22, no. 4, pp. 589–594, 1999. View at Publisher · View at Google Scholar · View at Scopus