摘要
导弹协同制导是提高中远距导弹作战效能的有效潜在途径之一。基于中远距雷达导弹中制导对载机的强依赖性问题,研究双机协同导弹中制导方法。首先,根据双机协同制导的原理建立双机协同制导的数学模型,给出修正指令的矢量计算方法;其次,对双机协同制导的误差进行建模分析,给出系统误差修正方法和随机误差计算方法;最后,对协同制导模型和制导精度进行仿真,仿真表明所建立协同中制导模型的可行性。
Missile cooperative guidance is one of effective potential method to enhance long-distance missile combat efficiency.In order to solve the problem that radar-guidance missile＇strengen dependency for air combat in mid-guidance,cooperative guidance method is given.Mathematic model of cooperative guidance are established based on cooperative guidance principle.Cooperated guidance command amendment vector computing method is derived based on vector computing rule.Cooperated missile guidance error is systematically analyzed.Both error amend method and random error computing method are established.At last,simulation are given,which proved the reliable of cooperative guidance model established in this paper.
出处
《火力与指挥控制》
CSCD
北大核心
2012年第12期59-63,共5页
Fire Control & Command Control
基金
航空科学基金资助项目(20095196012)
关键词
协同制导
修正指令
矢量计算
误差分析
目标截获概率
cooperative guidance
command amendment
vector compute
error analysis
target capture probability
