针对目前战斗部专家系统所存在的研制费用高、开发周期长等问题,借鉴先进的设计思想和战斗部威力计算模型,采用VC 6.0编程语言、OpenGL 3D API图形库和数据库技术,开发了一个战斗部可视化快速设计系统。该系统能实现对不同形状的杀爆战...针对目前战斗部专家系统所存在的研制费用高、开发周期长等问题,借鉴先进的设计思想和战斗部威力计算模型,采用VC 6.0编程语言、OpenGL 3D API图形库和数据库技术,开发了一个战斗部可视化快速设计系统。该系统能实现对不同形状的杀爆战斗部快速参数化建模、自动计算战斗部特征参数、破片威力参数等。最后以某一典型杀爆战斗部为例进行了验证。展开更多
The paper aimed to illustrate an idea about the feasibility of a peculiar aircraft, i.e., a 5th generation light fighter. At first, a short description of previous ＂generations＂ of jet fighter is given, introducing ...The paper aimed to illustrate an idea about the feasibility of a peculiar aircraft, i.e., a 5th generation light fighter. At first, a short description of previous ＂generations＂ of jet fighter is given, introducing the interest that has always been originated by the concept of＂light fighter＂ for every of the first four fighter generations. The derivation of the first idea of a new 5th generation light fighter is then described. Then to further investigate the feasibility of idea, a conceptual design study has been driven up by utilizing peculiar tools, both for quantitative and qualitative （i.e., the aircraft layout definition） evaluations. With the further support of preliminary study of subsystems, the result shows the feasibility of the concept.展开更多
文摘针对目前战斗部专家系统所存在的研制费用高、开发周期长等问题,借鉴先进的设计思想和战斗部威力计算模型,采用VC 6.0编程语言、OpenGL 3D API图形库和数据库技术,开发了一个战斗部可视化快速设计系统。该系统能实现对不同形状的杀爆战斗部快速参数化建模、自动计算战斗部特征参数、破片威力参数等。最后以某一典型杀爆战斗部为例进行了验证。
文摘The paper aimed to illustrate an idea about the feasibility of a peculiar aircraft, i.e., a 5th generation light fighter. At first, a short description of previous ＂generations＂ of jet fighter is given, introducing the interest that has always been originated by the concept of＂light fighter＂ for every of the first four fighter generations. The derivation of the first idea of a new 5th generation light fighter is then described. Then to further investigate the feasibility of idea, a conceptual design study has been driven up by utilizing peculiar tools, both for quantitative and qualitative （i.e., the aircraft layout definition） evaluations. With the further support of preliminary study of subsystems, the result shows the feasibility of the concept.
