유도탄의 유도명령 추종을 위한 혼합제어기 설계: 공력 및 측추력제어

Abstract

his paper is concerned with a mixed control with aerodynamic fm and side thrust control applied to an agile missile using a dynamic inversion and a time-varying control technique. The nonlinear dynamic inversion method with the weighting function allocates the desired control inputs(aerodynamic fin and side thrust control) to achieve a reference command, and the time-varying control technique plays the role to guarantee the robustness for the uncertainties. The proposed schemes are validated by nonlinear simulations with aerodynamic data