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• W2151093360 abstract "This paper is concerned with a mixed control with aerodynamic fin and side thrusters applied to an agile missile using dynamic inversion and the Extended-Mean Assignment (EMA) 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 EMA control technique guarantees the robustness for the uncertainties. The proposed schemes are validated by nonlinear simulations." @default.
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• W2151093360 date "2003-10-01" @default.
• W2151093360 modified "2023-09-22" @default.
• W2151093360 title "Autopilot design for agile missile with aerodynamic fin and side thruster" @default.
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• W2151093360 doi "https://doi.org/10.11499/sicep.2003.0_70_4" @default.
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