论文信息 - Robust mixed control with aerosurface and side thruster using LTV control technique

Robust mixed control with aerosurface and side thruster using LTV control technique

Abstract This paper is concerned with a mixed control with aerodynamic fin and side thrusters applied to an agile missile using two-time scale dynamic inversion and linear time-varying control technique. The nonlinear dynamic inversion method with the weighting function allocates the desired control inputs (aerodynamic fin and side thrusters) to track a reference trajectory, and the time-varying control technique guarantees the robustness for the uncertainties. Closed-loop stability is achieved by the assignment of the extended-mean of these linear time-varying eigenvalues to the left half complex plane. The proposed schemes are validated by nonlinear simulations

Jae Weon Choi | Ho Chul Lee | Yong Seok Choi

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