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针对发动机推力方向与轴线方向垂直的战术导弹,建立其在大攻角情况下攻击地面固定目标的数学模型,然后应用非线性控制理论设计了一种非线性导引规律,仿真的结果表明效果良好。
Aiming at the tactical missile with the thrust direction of the engine perpendicular to the axial direction, a mathematical model of attacking ground fixed target under a large angle of attack is established. Then a nonlinear guidance law is designed based on the nonlinear control theory. The simulation results show that the effect is good .