摘要
从经典斜抛运动入手,加入并考虑气动阻力影响,从能量学的角度分析上仰投放对制导滑翔炸弹射程的影响,并通过基于制导滑翔炸弹的气动特性和运动数学模型进行验证。
Starting from the analysis of projectile motion, and to consider adding the aerodynamic drag, based on the energy conservation law, changes in the range of Projectile launch Guided glide bomb is analysed, and verified by simulation.
出处
《科学技术与工程》
2011年第23期5603-5607,共5页
Science Technology and Engineering
关键词
制导滑翔炸弹
斜抛运动
能量法
射程
guided glide projectile motion law of energy conservation range
