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International Journal of Aerospace Engineering
Volume 2016, Article ID 6598983, 11 pages
http://dx.doi.org/10.1155/2016/6598983
Research Article

Three-Dimensional Integrated Guidance and Control for Near Space Interceptor Based on Robust Adaptive Backstepping Approach

1School of Astronautics, Harbin Institute of Technology, Harbin 150001, China
2Shenyang Aircraft Design & Research Institute, Shenyang 110035, China

Received 17 April 2016; Revised 5 October 2016; Accepted 12 October 2016

Academic Editor: Kenneth M. Sobel

Copyright © 2016 Changsheng Gao 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. R. H. Chen, J. L. Speyer, and D. Lianos, “Optimal intercept missile guidance strategies with autopilot lag,” Journal of Guidance, Control, and Dynamics, vol. 33, no. 4, pp. 1264–1272, 2010. View at Publisher · View at Google Scholar · View at Scopus
  2. S. S. Moosapour, G. Alizadeh, S. Khanmohammadi, and H. Moosapour, “A novel robust proportional navigation guidance law design for missile considering autopilot dynamic,” Transactions of the Institute of Measurement and Control, vol. 35, no. 5, pp. 703–710, 2013. View at Publisher · View at Google Scholar · View at Scopus
  3. W. Shang, J. Guo, S. Tang, Y. Ma, and Y. Zhang, “Impact time guidance law considering autopilot dynamics based on variable coefficients strategy for maneuvering target,” Mathematical Problems in Engineering, vol. 2015, Article ID 815149, 10 pages, 2015. View at Publisher · View at Google Scholar · View at Scopus
  4. D. Chwa and J. Y. Choi, “Adaptive nonlinear guidance law considering control loop dynamics,” IEEE Transactions on Aerospace and Electronic Systems, vol. 39, no. 4, pp. 1134–1143, 2003. View at Publisher · View at Google Scholar · View at Scopus
  5. B. Xu and D. Zhou, “Three dimensional adaptive dynamic surface guidance law accounting for autopilot lag,” in Proceedings of the American Control Conference (ACC '14), pp. 578–583, IEEE, Portland, Ore, USA, June 2014. View at Publisher · View at Google Scholar · View at Scopus
  6. P. P. Qu and D. Zhou, “A dimension reduction observer-based guidance law accounting for dynamics of missile autopilot,” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 227, no. 7, pp. 1114–1121, 2013. View at Publisher · View at Google Scholar · View at Scopus
  7. G.-L. Li, H. Yan, and H.-B. Ji, “A guidance law with finite time convergence considering autopilot dynamics and uncertainties,” International Journal of Control, Automation and Systems, vol. 12, no. 5, pp. 1011–1017, 2014. View at Publisher · View at Google Scholar · View at Scopus
  8. S. M. He and D. F. Lin, “Continuous composite finite-time convergent guidance laws with autopilot dynamics compensation,” ISA Transactions, vol. 58, pp. 270–278, 2015. View at Publisher · View at Google Scholar · View at Scopus
  9. P. Qu, C. Shao, and D. Zhou, “Finite time convergence guidance law accounting for missile autopilot,” Journal of Dynamic Systems, Measurement and Control, Transactions of the ASME, vol. 137, no. 5, Article ID 051014, pp. 1–8, 2015. View at Publisher · View at Google Scholar · View at Scopus
  10. Z. X. Zhang, S. H. Li, and S. Luo, “Composite guidance laws based on sliding mode control with impact angle constraint and autopilot lag,” Transactions of the Institute of Measurement and Control, vol. 35, no. 6, pp. 764–776, 2013. View at Publisher · View at Google Scholar · View at Scopus
  11. S. He, D. Lin, and J. Wang, “Robust terminal angle constraint guidance law with autopilot lag for intercepting maneuvering targets,” Nonlinear Dynamics, vol. 81, no. 1-2, pp. 881–892, 2015. View at Publisher · View at Google Scholar · View at Scopus
  12. D. Zhou, P. P. Qu, and S. Sun, “A guidance law with terminal impact angle constraint accounting for missile autopilot,” Journal of Dynamic Systems, Measurement and Control, vol. 135, no. 5, Article ID 051009, pp. 1–10, 2013. View at Publisher · View at Google Scholar · View at Scopus
  13. 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 MathSciNet · View at Scopus
  14. M. F. Jegarkandi, A. Ashrafifar, and R. Mohsenipour, “Adaptive integrated guidance and fault tolerant control using backstepping and sliding mode,” International Journal of Aerospace Engineering, vol. 2015, Article ID 253478, 7 pages, 2015. View at Publisher · View at Google Scholar · View at Scopus
  15. S. Xingling and W. Honglun, “Back-stepping active disturbance rejection control design for integrated missile guidance and control system via reduced-order ESO,” ISA Transactions, vol. 57, pp. 10–22, 2015. View at Publisher · View at Google Scholar
  16. A. Zhurbal and M. Idan, “Effect of estimation on the performance of an integrated missile guidance and control system,” IEEE Transactions on Aerospace and Electronic Systems, vol. 47, no. 4, pp. 2690–2708, 2011. View at Publisher · View at Google Scholar · View at Scopus
  17. H. Yan and H. Ji, “Integrated guidance and control for dual-control missiles based on small-gain theorem,” Automatica, vol. 48, no. 10, pp. 2686–2692, 2012. View at Publisher · View at Google Scholar · View at MathSciNet · View at Scopus
  18. K. Chen, B. Fu, Y. Ding, and J. Yan, “Integrated guidance and control method for the interception of maneuvering hypersonic vehicle based on high order sliding mode approach,” Mathematical Problems in Engineering, vol. 2015, Article ID 648231, 19 pages, 2015. View at Publisher · View at Google Scholar · View at Scopus
  19. S. Shamaghdari, S. K. Nikravesh, and M. Haeri, “Integrated guidance and control of elastic flight vehicle based on robust MPC,” International Journal of Robust and Nonlinear Control, vol. 25, no. 15, pp. 2608–2630, 2015. View at Publisher · View at Google Scholar · View at MathSciNet · View at Scopus
  20. M.-Z. Hou and G.-R. Duan, “Adaptive dynamic surface control for integrated missile guidance and autopilot,” International Journal of Automation and Computing, vol. 8, no. 1, pp. 122–127, 2011. View at Publisher · View at Google Scholar · View at Scopus
  21. X. L. Liang, M. Z. Hou, and G. R. Duan, “Adaptive dynamic surface control for integrated missile guidance and autopilot in the presence of input saturation,” Journal of Aerospace Engineering, vol. 28, no. 5, Article ID 04014121, pp. 1–8, 2015. View at Publisher · View at Google Scholar · View at Scopus
  22. F. Wang, G. Liu, and X.-G. Liang, “Integrated guidance and control design for the near space interceptor,” International Journal of Aeronautical and Space Sciences, vol. 16, no. 2, pp. 278–294, 2015. View at Publisher · View at Google Scholar · View at Scopus
  23. H. T. Song, T. Zhang, G. L. Zhang, and C. J. Lu, “Integrated interceptor guidance and control with prescribed performance,” International Journal of Robust and Nonlinear Control, vol. 25, no. 16, pp. 3179–3194, 2015. View at Publisher · View at Google Scholar · View at MathSciNet · View at Scopus
  24. 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
  25. 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
  26. C. Guo and X.-G. Liang, “Integrated guidance and control based on block backstepping sliding mode and dynamic control allocation,” Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering, vol. 229, no. 9, pp. 1559–1574, 2015. View at Publisher · View at Google Scholar · View at Scopus
  27. H. T. Song, T. Zhang, and G. L. Zhang, “L1 adaptive state feedback controller for three-dimensional integrated guidance and control of interceptor,” Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering, vol. 228, no. 10, pp. 1693–1701, 2014. View at Publisher · View at Google Scholar · View at Scopus
  28. Y. A. Hu, Y. Q. Jin, and H. Y. Li, Robustness of Adaptive Backstepping Control for Nonlinear Systems, Publishing House of Electronics Industry, Beijing, China, 2010.
  29. J. Q. Han, Active Disturbance Rejection Control Technique-The Technique for Estimating and Compensating the Uncertainties, National Defense Industry Press, 2009.
  30. X. F. Qian, R. X. Lin, and Y. N. Zhao, Flight Dynamics of Missile, Beijing Institute of Technology Press, Beijing, China, 2008.
  31. D. Zhou, New Guidance Laws for Homing Missile, National Defense Industry Press, 2002.