An elastic vibration model for high length diameter ratio spinning rocket with attitude control system which can be used for trajectory simulation is established. The basic theory of elastic dynamics and vibration dy...An elastic vibration model for high length diameter ratio spinning rocket with attitude control system which can be used for trajectory simulation is established. The basic theory of elastic dynamics and vibration dynamics were both used to set up the elastic vibration model of rocket body. In order to study the problem more conveniently, the rocket's body was simplified to be an even beam with two free ends. The model was validated by simulation results and the test data.展开更多
The dynamics of a coupled rigid-flexible rocket launcher is reported. The coupled rigid-flexible rocket launcher is divided into two subsystems, one is a system of rigid bodies, the other a flexible launch tube which ...The dynamics of a coupled rigid-flexible rocket launcher is reported. The coupled rigid-flexible rocket launcher is divided into two subsystems, one is a system of rigid bodies, the other a flexible launch tube which can undergo large overall motions spatially. First, the mathematical models for these two subsystems were established respectively. Then the dynamic model for the whole system was obtained by considering the coupling effect between these two subsystems. The approach, which divides a complex system into several simple subsystems first and then obtains the dynamic model for the whole system via combining the existing dynamic models for simple subsystems, can make the modeling procedure efficient and convenient.展开更多
弹箭产品的多视图物料清单XBOM(X bill of material)是多利益攸关方从不同寿命阶段的结构组成、数据信息以及交互流程等角度对弹箭产品的全方位基础支持文件。对弹箭产品XBOM数据进行管理,统筹管控全寿命周期内的数据,可消除不同寿命阶...弹箭产品的多视图物料清单XBOM(X bill of material)是多利益攸关方从不同寿命阶段的结构组成、数据信息以及交互流程等角度对弹箭产品的全方位基础支持文件。对弹箭产品XBOM数据进行管理,统筹管控全寿命周期内的数据,可消除不同寿命阶段相关方、业务及数据间的交互脱节及单向传递,为弹箭产品实现全数字模型供应提供有效数据源支持。为满足面向弹箭产品XBOM数据的有机集成及多方协同需求,提出了基于数字主线的弹箭产品XBOM数据管理体系和方法。通过剖析数字主线框架,提出并建立了基于数字主线的弹箭产品XBOM数据管理体系。以“数据-交互-建模-应用”的体系层次为指导,提出了基于数字主线的弹箭产品XBOM数据管理方法,包含数据组织、数据关联关系分析、数据建模及数据应用。以某型运载火箭结构系统为对象,开发基于数字主线的弹箭产品XBOM数据管理体系并进行了应用验证。文中所提出体系和方法为实现弹箭产品XBOM数据管控、集成及共享提供具体指导,有利于促进我国弹箭产品全寿命周期数据管理系统的发展。展开更多
The research on multiple launch rocket system(MLRS)is now even more demanding in terms of reducing the time for dynamic calculations and improving the firing accuracy,keeping the cost as low as possible.This study emp...The research on multiple launch rocket system(MLRS)is now even more demanding in terms of reducing the time for dynamic calculations and improving the firing accuracy,keeping the cost as low as possible.This study employs multibody system transfer matrix method(MSTMM),to model MLRS.The use of this method provides effective and fast calculations of dynamic characteristics,initial disturbance and firing accuracy.Further,a new method of rapid extrapolation of ballistic trajectory of MLRS is proposed by using the position information of radar tests.That extrapolation point is then simulated and compared with the actual results,which demonstrates a good agreement.The closed?loop fire correction method is used to improve the firing accuracy of MLRS at low cost.展开更多
文摘An elastic vibration model for high length diameter ratio spinning rocket with attitude control system which can be used for trajectory simulation is established. The basic theory of elastic dynamics and vibration dynamics were both used to set up the elastic vibration model of rocket body. In order to study the problem more conveniently, the rocket's body was simplified to be an even beam with two free ends. The model was validated by simulation results and the test data.
文摘The dynamics of a coupled rigid-flexible rocket launcher is reported. The coupled rigid-flexible rocket launcher is divided into two subsystems, one is a system of rigid bodies, the other a flexible launch tube which can undergo large overall motions spatially. First, the mathematical models for these two subsystems were established respectively. Then the dynamic model for the whole system was obtained by considering the coupling effect between these two subsystems. The approach, which divides a complex system into several simple subsystems first and then obtains the dynamic model for the whole system via combining the existing dynamic models for simple subsystems, can make the modeling procedure efficient and convenient.
文摘弹箭产品的多视图物料清单XBOM(X bill of material)是多利益攸关方从不同寿命阶段的结构组成、数据信息以及交互流程等角度对弹箭产品的全方位基础支持文件。对弹箭产品XBOM数据进行管理,统筹管控全寿命周期内的数据,可消除不同寿命阶段相关方、业务及数据间的交互脱节及单向传递,为弹箭产品实现全数字模型供应提供有效数据源支持。为满足面向弹箭产品XBOM数据的有机集成及多方协同需求,提出了基于数字主线的弹箭产品XBOM数据管理体系和方法。通过剖析数字主线框架,提出并建立了基于数字主线的弹箭产品XBOM数据管理体系。以“数据-交互-建模-应用”的体系层次为指导,提出了基于数字主线的弹箭产品XBOM数据管理方法,包含数据组织、数据关联关系分析、数据建模及数据应用。以某型运载火箭结构系统为对象,开发基于数字主线的弹箭产品XBOM数据管理体系并进行了应用验证。文中所提出体系和方法为实现弹箭产品XBOM数据管控、集成及共享提供具体指导,有利于促进我国弹箭产品全寿命周期数据管理系统的发展。
基金supported by the Na- tional Natural Science Foundation of China (No. 11472135)the Science Challenge Project (No. JCKY2016212A506- 0104)
文摘The research on multiple launch rocket system(MLRS)is now even more demanding in terms of reducing the time for dynamic calculations and improving the firing accuracy,keeping the cost as low as possible.This study employs multibody system transfer matrix method(MSTMM),to model MLRS.The use of this method provides effective and fast calculations of dynamic characteristics,initial disturbance and firing accuracy.Further,a new method of rapid extrapolation of ballistic trajectory of MLRS is proposed by using the position information of radar tests.That extrapolation point is then simulated and compared with the actual results,which demonstrates a good agreement.The closed?loop fire correction method is used to improve the firing accuracy of MLRS at low cost.
