空空导弹制导精度仿真评估系统设计  

Design on Air-to-air Missile Guidance Accuracy Simulation and Evaluation System

作　　者：孟博[1] MENG Bo(China Airborne Missile Academy,Luoyang 471000)

机构地区：[1]中国空空导弹研究院,洛阳471000

出　　处：《舰船电子工程》2022年第10期93-95,109,共4页Ship Electronic Engineering

摘　　要：制导精度是空空导弹的关键性能指标。论文基于空空导弹制导精度仿真数学模型,开展了架构功能规划、接口匹配设计、系统集成优化、软件实现调试,完成了空空导弹制导精度仿真评估系统设计,系统创新实现不同作战模式、不同仿真模式、不同目标、不同误差等丰富条件下的单条弹道/批量弹道的单次/多次弹道仿真及制度精度评估,可解决传统制导精度仿真评估功能单一的局限和不足,进一步丰富和拓展制度精度仿真评估的全面性和有效性。Guidance accuracy is key performance index of air-to-air missile. Based on missile guidance accuracy simulation mathematical model,the air-to-air missile guidance accuracy simulation and evaluation system is constructed by architecture function planning,interface matching design,system integrated implementation and software implementation debugging. The system could innovatively simulate ballistic and evaluate guidance accuracy in single ballistic or batch ballistics separately and largely in rich conditions which contain different combat patterns,different simulation patterns,different target,different error. The traditional guidance accuracy simulation and evaluation is lack of functionality and the limitation and deficiency is solved. The completeness and effectiveness of air-to-air missile guidance accuracy simulation and evaluation is enriched and expanded furtherly.

关 键 词：空空导弹 制导精度 仿真评估系统 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]