CAJ | 학술논문

研究了在滑翔弹道的波峰加载水平推力对射程的影响问题。针对动力滑翔导弹建立其弹道运动模型,利用M atlab对其进行仿真。结果表明,加载动力后导弹射程增益明显。
연구료재활상탄도적파봉가재수평추력대사정적영향문제。침대동력활상도탄건립기탄도운동모형,이용M atlab대기진행방진。결과표명,가재동력후도탄사정증익명현。
Glide missile is now the new missile that all countries are researching on,and loading power in the process of gliding can add even more range and penetration of missiles.This article is to study effects on range of missiles when loading power on the peak of trajectory.Trajectory design plays a very important role overall design of the missile,in this paper it has established its trajectory motion model of dynamic-glider missile and simulated its trajectory using MATLAB software.The results show that the missile has significantly a range gain after loading power.