摘要
针对对策法的不足，引入类比例导引法和优化指向向量法，建立了两种方法的数学模型，分析了它们的导引性能，数字仿真结果表明这两种方法不但在执行速度上有很大提高，而且在一定条件下弥补了对策法的缺陷。并据此进一步提出了在现有知识的基础上将多种方法结合起来以提高飞机作战效能的观点。
To cope with the shortages of matrix game, mathematical models of quasi proportional guidance and optimal heading vector are constructed, which are used successfully in multiple aircraft air to air combat simulation. Numerical examples illustrate that the introduction of the later two ways leads to a significant decrease in the implementational burden, and retrieves some defects of the matrix game. Since the two new ways also have their shortcomings, the merits of many guidances should be synthesized to increase the effectiveness of a fighter.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1997年第3期371-374,共4页
Acta Aeronautica et Astronautica Sinica
基金
航空科学基金
关键词
机动决策
矩阵对策
类比例导引
战斗机
空战
maneuvering decision, optimal heading vector, matrix game, quasi proportional guidance
