NON-SMOOTH DESIGN FOR SYSTEMS WITH HETEROGENEOUS MULTIPLE ACTUATORS

Kemao Ma

References

  1. [1] A. Al-Mamun, T. Suthasun, S.M. Sri-Jayantha, and T.H. Lee, Multirate controller for dual actuated servomechanism in hard disk drive, Control and Intelligent Systems, 42(4), 2014, 271–278.
  2. [2] C. Restrepo and J. Valasek, Preliminary study using forward reaction control system jets during space shuttle entry, AIAA Guidance, Navigation and Control Conf. and Exhibit, AIAA Paper No. 2006-6073, Keystone, CO, 2006, 1–10.
  3. [3] D. Taur and H. Hsu, A composite guidance strategy for SAAMM with side jet controls, AIAA Guidance, Navigation and Control Conf. and Exhibit, AIAA Paper No. 2001-4427, Montreal, Canada, 2001, 1–13.
  4. [4] P. Menon and P. Iragavarapu, Adaptive techniques for multiple actuator blending, AIAA Guidance, Navigation and Control Conf. and Exhibit, AIAA Paper No. 1998-4494, Boston, MA, 1998, 1–12.
  5. [5] C. Tournes, Y. Shtessel, and H. Shkolnikov, Missile controlled by lift and divert thrusters using nonlinear dynamic sliding manifolds, Journal of Guidance, Control, and Dynamics, 29(3), 2006, 617–625.
  6. [6] V. Rajendran and S. Mahalingam, Optimal allocation and sizing of facts controllers using differential evolution algorithm, Control and Intelligent Systems, 41(3), 2013, 136–142.
  7. [7] D. Mokeddem and A. Khellaf, Simultaneous fault tolerance analysis of actuators and sensors application to a five tank systems, Control and Intelligent Systems, 36(2), 2008, 169–173.
  8. [8] F. He, K. Ma, and Yao, Firing logic optimization design of lateral jets in missile attitude control systems, 17th International Conf. of Control Applications, San Antonio, TX, August 2008, 936–941.
  9. [9] F. He, D. Ji, K. Ma, and Y. Yao, Switching logic design based on finite-time gain measure for a flight vehicle with multiple actuators, 2009 IEEE Aerospace Conf., Big Sky, MT, March 2009, 1–5.
  10. [10] Q. Wang, B. Yang, and K. Ma, PWPF optimizing design and its application research to terminal guidance of kinetic killing vehicle, Journal of Astronautics, 26(5), 2005, 576–580.
  11. [11] Y. Shtessel, C. Tournes, and I. Shkolnikov, Guidance and autopilot for missiles steered by aerodynamic lift and divert thrusters using second order sliding modes, AIAA Guidance, Navigation and Control Conf. and Exhibit, AIAA Paper No. 2006-6784, Keystone, CO, 2006, 1–22.
  12. [12] K. Ma and H. Zhao, Sliding modes control design for a class of systems with multiple actuators and its applications, Control Theory & Applications, 28(4), 2011, 556–560.
  13. [13] Z. Shi, W. Ma, and Y. Zhang, A novel control system design method for missile with lateral jet and aerodynamic surfaces, Fourth International Conf. on Intelligent Control and Information Processing (ICICIP), Beijing, China, June 9–11, 2013, 858–861.
  14. [14] C.H. Tinh, V.H. Tien, N.C. Dinh, and M.N. Anh, Design of Takagi-Sugeno fuzzy controller for automatic stabilization system of missiles with blended aerodynamic and lateral impulsive reaction-jet, Seventh IEEE Symposium on Computational Intelligence for Security and Defense Applications(CISDA), Hanoi, Vietnam, December 14–17, 2014, 1–7.
  15. [15] H.K. Khalil, Nonlinear systems, 3rd ed. (Upper Saddle River, NJ: Prentice Hall, 2002).
  16. [16] S. Bhat and D. Bernstein, Finite-time stability of continuous autonomous systems, SIAM Journal of Control and Optimization, 38(3), 2000, 751–766.
  17. [17] A. Levant, Higher-order sliding modes, differentiation and output-feedback control,International Journal of Control, 76(9/10), 2003, 924–941.
  18. [18] X. Qian, R. Lin, and Y. Zhao, Flight dynamics of missiles (Beijing, China: Beijing Institute of Technology Press, 2006).
  19. [19] S. Sastry, Nonlinear systems: Analysis, stability, and control (New York, NY: Springer-Verlag, 1999).
  20. [20] K. Ma, H. Zhao, and D. Zhang, Control design and implementation for missiles with blended lateral jets and aerodynamic control systems, Journal of Astronautics, 32(2), 2011, 310–316.

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