CAJ | 학술논문

针对采用地面滑轨倾斜发射方式的导弹,根据发射模型的特点,建立发射动力学模型,推导其离轨发射运动方程组,对"一"字型滑轨与"品"字型滑轨,分别取不同的导轨长度和发射倾角进行仿真计算,得到导弹离轨运动参数和离轨运动规律,结果表明,导弹的离轨运动特性与滑轨长度和发射倾角有关,此外,对于"一"字型滑轨,还须考虑导弹离轨时的下沉问题.
침대채용지면활궤경사발사방식적도탄,근거발사모형적특점,건립발사동역학모형,추도기리궤발사운동방정조,대"일"자형활궤여"품"자형활궤,분별취불동적도궤장도화발사경각진행방진계산,득도도탄리궤운동삼수화리궤운동규률,결과표명,도탄적리궤운동특성여활궤장도화발사경각유관,차외,대우"일"자형활궤,환수고필도탄리궤시적하침문제.
According to the characteristics of launch model, launch dynamics model was founded, and launch movement equations were deduced for missile of tiltable launch. Different slide lengths and launch obliquities were used to simulate and calculate for straight line slides and triangle slides. Movement parameters and laws of the missile were got. The results show that off-slide movement of missile is related to slide lengths and launch obliquities. In addition, subsidence of missile must be considered for triangle slides.