摘要
为探求临近空间无动力攻击器运动参数的解析模型,采用均匀设计试验方法,以攻击器发射参数为设计变量,从设计空间中选择一些特定的设计点,构造了临近空间攻击器速度、射程以及飞行时间的响应面模型。通过仿真算例,对各响应面模型分别进行显著性检验,证明了所建立的响应面都具有较高的近似精度。
In order to acquire the Response Surface Model of velocity, fire range and flight time of near space unpowered guided bomb, uniform design experimentation is used, and the fire parameters, such as fire velocity, fire angle, and fire height are chosen as the design variables. The significance of the Response Surface Models is tested through the emulation example. It indicates that all the models are of high precision.
出处
《军械工程学院学报》
2009年第5期24-27,共4页
Journal of Ordnance Engineering College
关键词
临近空间
无动力攻击器
运动参数
均匀设计
响应面模型
near space
unpowered guided bomb
kinetic parameters
uniform design
response surface model ( RSM )