A Robust Recursive Control Approach to Nonlinear Missile Autopilot

강인 반복 제어를 이용한 비선영 유도탄 자동조종장치

  • Published : 2001.12.01

Abstract

In this paper, a robust recursive control approach for nonlinear system, which is based on Lyapunov stability, is proposed. The proposed method can apply to extended systems including cascaded systems and the stability is guaranteed in the sense of Lyapunov. The recursive design procedure so called “robust recursive control approach” is used to find a stabilizing robust controller and simultaneously estimate the uncertainty parameters. First, a nonlinear model with uncertainties whose bounds are unknown is derived. Then, unknown bounds of uncertainties are estimated. By using these estimates, the stabilizing robust controller is updated at each step. This approach is applied to the pitch autopilot design of a nonlinear missile system and simulation results indicate good performance.

Keywords

References

  1. I. Kanellakopoulos, P. V. Kokotovic, and A. S. Morse, 'Systematic design of adaptive controllers for feedback Linearizable system,' IEEE Trans. on Automatic Control, vol. 36, pp. 1241-1253, 1991 https://doi.org/10.1109/9.100933
  2. M. Krstic, I. Kanellakopoulos, and P. V. Kokotovic, Nonlinear and Adaptive Control Design, John Wiley & Sons, 1995
  3. M. M. Polycarpou and P. A. Ioannou, 'A robust adaptive nonlinear control design,' Automatica, vol. 32, no. 3, pp. 423-427, 1996 https://doi.org/10.1016/0005-1098(95)00147-6
  4. R. A. Hull and Z. Qu, 'Dynamic robust recursive control design and its application to a nonlinear missile autopilot,' Proc. of American Control Conference, pp. 833-837, 1997 https://doi.org/10.1109/ACC.1997.611921