摘要
从研究无动力滑翔弹的可攻击区大小及相应的6-D飞行轨迹角度出发,基于无动力滑翔弹运动学与动力学和中/末制导律的数学模型,通过不同初始投放条件的组合(投放高度、投放速度、投放角度),计算了大量的可攻击区及相应的6-D飞行轨迹,比较了不同组合情况下的可攻击区大小及相应的6-D飞行轨迹,得出了一组无动力滑翔弹最优初始投放条件数据。
Initial release conditions of the no-power gliding bomb were optimized based on flight simulation models of the missile, including differential flight dynamics equations and the medium/terminal guidance laws. The performance index is maximizing attack zone. A lot of attack zones ( and their 6-D flight trajectories) of the no-power bomb were calculated based on different combinations of initial releasing conditions ( height above sea level, velocity and path angles), so the optimal release conditions were gotten by a great deal of flight numerical simulation on attack zones.
出处
《飞行力学》
CSCD
北大核心
2009年第1期93-96,共4页
Flight Dynamics