| ID | 原文 | 译文 |
| 10114 | 对时延容忍范围的仿真与分析可为实际战术数据链设计提供一定指导意义。 | The delay tolerance range of the simulation and analysis for the actual tactical data link is designed to provide a certain guiding significance. |
| 10115 | 对由混合数据、多类型的赋权方法、多结构的集结方式等组成的广义混合型决策信息,研究该类决策信息的综合集成和求解问题。 | Methods to empowerment by mixed data, multi-type, way of gathering more structure composed of generalized hybrid decision information, research the class of the integrated decision information and solve problems. |
| 10116 | 首先以传统的决策流程为底层框架,对广义混合型决策信息进行分类整合,构建信息集成框架; | In the first place in the traditional decision-making process as the underlying framework, classifying the generalized mixed decision-making information integration, information integration framework. |
| 10117 | 然后,从随机模拟视角分析了信息集成框架的求解方法并归纳了求解的基本步骤。 | Then, from the perspective of stochastic simulation method of information integration framework and summarizes the basic steps of solving. |
| 10118 | 在此基础上,通过导弹方案的选择问题对本文给出方法的具体应用进行了说明,并验证了该方法的有效性。 | On this basis, through the missile scheme selection problem of the practical application illustrates the method presented in this paper, and verify the effectiveness of the proposed method. |
| 10119 | 本文通过构建信息集成框架的方式解决了多类型决策信息的融合难题,且实现了信息集成框架的柔性求解。 | In this paper, through the way of information integration framework solves the problem many model of decision information fusion, and realizes information integration framework of flexible solution. |
| 10120 | 该研究可为民主决策中多来源、多类型决策信息的融合提供技术参考。 | The study can provide multiple sources in the democratic decision-making, multi-type decision information fusion to provide technical reference. |
| 10121 | 为了实现复杂航天器导航、制导与控制(guidance navigation and control,GNC)系统的快速设计与仿真验证,加快GNC系统从算法设计到产品实现的过程,解决数字仿真与实物仿真一致性的问题,提出了一种基于星载软件在环的GNC快速原型仿真系统。 | In order to achieve the complex spacecraft navigation, guidance and control (guidance navigation and control, GNC) system of rapid design and simulation verification, to speed up the GNC system from algorithm design to product realization process, solve the problem of the consistency of digital simulation and physical simulation, this paper proposes a spaceborne software based on ring of GNC simulation system for fast prototyping. |
| 10122 | 通过虚拟GNC计算机处理器内核和硬件接口的方式实现星载GNC计算机原型,解决了快速原型仿真系统GNC软件代码与实物星载计算机软件代码的一致性; | Through virtual GNC computer processor core and hardware interface for spaceborne GNC computer prototype, the way of solving the GNC rapid prototyping simulation system software code and physical consistency of satellite-borne computer software code; |
| 10123 | 利用Simulink/Matlab进行航天器动力学/运动学建模和GNC系统测量部件及执行部件的数字化建模,基于实时扩展(real time extension,RTX)系统和功能硬件板卡实现数字化模型与实物的转化,解决数字仿真与实物仿真GNC系统内部接口特性、时序和逻辑一致性的问题。 | Using Simulink/Matlab, the measurement of spacecraft dynamics/kinematics modeling and GNC system components and execute component of digital modeling, based on real-time extension (real time extension, RTX) system and achieve the conversion of digital model and the physical function of hardware interface card, digital simulation and physical simulation GNC system internal interface features, timing, and logic consistency problem. |