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1 results

  • Sliding mode-based continuous guidance law with terminal angle constraint

  • S. He, D. Lin
  • Journal:
    The Aeronautical Journal / Volume 120 / Issue 1229 / July 2016
    Published online by Cambridge University Press:
    07 June 2016, pp. 1175-1195

  • In this paper, sliding mode control and disturbance observer are used to design a new continuous composite guidance law with terminal angle constraint. The robustness and finite-time convergence of the proposed guidance law is established using the Lyapunov stability theory. For performance improvement, a nonlinear disturbance observer, which can be viewed as a ‘patch’ for the original guidance law, is designed to estimate the target manoeuvre. Theoretical analysis and simulation results demonstrate the effectiveness of the proposed method.