摘要
建立激光制导炸弹空间六自由度运动方程组,激光制导炸弹控制系统数学模型和控制信号的形成模型,用拟合技术求解气动力因数。仿真计算了水平投放时的投放域,对影响制导精度的因素进行了分析。
This paper establishes the boss's six-freedom space movement differential equations,control system mathematical model and control signal formation model.The approach technology is taken use of to solve get the coefficient of pneumatic force.By calculation and simulation,the bomb's toss area in horizon has been got.Factors affecting the boundary of toss area are also been analyzed.
出处
《弹箭与制导学报》
CSCD
北大核心
2003年第S6期70-73,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
激光制导炸弹
气动力
投放域
aser-guided bomb
toss area
pneumatic force
