火力与指挥控制2012，Vol.37Issue(12)：59-63,5.
双机协同导弹指令修正中制导技术
Research on Command Amendment Guidance Method of Double-Fighter Cooperative Missile Guidance
摘要
Abstract
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.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Key words
cooperative guidance/command amendment/vector compute/error analysis/target capture probability分类
军事科技引用本文复制引用
付昭旺,于雷,李战武,徐安..双机协同导弹指令修正中制导技术[J].火力与指挥控制,2012,37(12):59-63,5.基金项目
航空科学基金资助项目(20095196012) （20095196012）
