CAJ | 학술논문

针对现代导弹武器多约束、高精度制导的基本要求，在综合考虑带落角和末端攻角约束的条件下，用二次型最优控制推导出一种新的最优末制导律。仿真结果表明，该末制导律既能够满足高精度制导的要求，同时也能够满足对落角和末端攻角的控制要求。
침대현대도탄무기다약속、고정도제도적기본요구，재종합고필대락각화말단공각약속적조건하，용이차형최우공제추도출일충신적최우말제도률。방진결과표명，해말제도률기능구만족고정도제도적요구，동시야능구만족대락각화말단공각적공제요구。
In order to meet the requirements of the missile high-precision guilded. The considering the condi-tions under the constraints with the impact angle and the angle of attack, the new guidance law was deduced by the quadratic optimal control. The verified results showed that the guidance law with the impact angle and the angle of attack constraint was satisfied not only the requirements of high-precision guidance, but also the end of attack could be a good control.