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Integrated Guidance and Control with Input Saturation and Impact Angle Constraint

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  • Zhenhua Fu
  • Kuanqiao Zhang
  • Qintao Gan
  • Suochang Yang

Abstract

Aiming at the problem of impact angle constraint and input saturation, an integrated guidance and control (IGC) algorithm with impact angle constraint and input saturation is proposed. A three-channel independent design model of missile IGC with impact angle constraint is established, and an extended state observer with fast finite-time convergence is designed to estimate and compensate model errors and coupling relationship between channels. Based on the nonsingular terminal sliding mode control and backstepping control, the IGC three-channel independent design is completed. Nussbaum function and an auxiliary system are introduced to deal with the input saturation. The Lyapunov function is constructed to prove the finite-time convergence of the IGC algorithm. The missile six-degree-of-freedom simulation results show the effectiveness and superiority of the IGC algorithm.

Suggested Citation

  • Zhenhua Fu & Kuanqiao Zhang & Qintao Gan & Suochang Yang, 2020. "Integrated Guidance and Control with Input Saturation and Impact Angle Constraint," Discrete Dynamics in Nature and Society, Hindawi, vol. 2020, pages 1-19, September.
  • Handle: RePEc:hin:jnddns:5917983
    DOI: 10.1155/2020/5917983
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