To meet the need of combat effectiveness analysis of air-to-surface missile, a scheme of missile combat effective simulation system based on distributed interactive simulation was proposed. 针对现代空面导弹武器系统作战效能分析的任务和功能需求,基于分布交互仿真的思想,开发了一套分布交互式的空面导弹作战效能仿真系统。
The paper first analyzes the characteristic on guidance of air-to-surface missile, and establishes relative aerodynamics model of missile and target. 分析了空对面导弹导引过程的特点,建立了导弹与目标的相对运动关系模型。
In order to study the terminal precision guidance of the hypersonic air-to-surface missile with constraints, the guidance law was designed respectively in the pitching plane and swerve plane. 针对高超声速空地导弹多约束高精度末制导的基本需求,在三维解耦的俯仰平面和转弯平面上分别设计制导律。
Modeling and Simulation of Air-to-Surface Missile(ASM) System 空面导弹系统的建模与仿真
Research on Integrated Model of Evaluating Combat Effectiveness for Air-to-surface Missile Weapon Systems 空地导弹武器系统作战效能综合分析模型研究