CAJ | 학술논문

根据火箭弹的轨迹方程分析了火箭弹射程的影响因素，描述了分离式制导火箭弹的原理以及制导控制方法，选取不同初始速度及升阻比参数进行了大攻角增程效果的仿真分析。结果表明，采用大升阻比实现火箭弹大攻角增程方法可以有效实现火箭弹增程。
근거화전탄적궤적방정분석료화전탄사정적영향인소，묘술료분리식제도화전탄적원리이급제도공제방법，선취불동초시속도급승조비삼수진행료대공각증정효과적방진분석。결과표명，채용대승조비실현화전탄대공각증정방법가이유효실현화전탄증정。
The influence factors about the range of rocket is analysed according to the rocket’s traj-equation. The principle of the warhead-separating guided rocket and the design of its guidance and control law is described. The effect of range-extending under large angle of attack is studied under different initial velocities and lift-drag ratios. The result indicates the technology of extending range under large angle of attack with a high lift-drag ratio is valid.