ID 原文 译文
9844 在此基础上,进一步考虑了INS/全球定位系统(global positioning system,GPS)组合导航时该方法的改进算法,提出了一种利用GPS定位信息和预测滤波器对飞行器动力学模型误差估计的方法。 ‭On this basis, further consider the INS/GPS (global positioning system, GPS) integrated navigation when the method of improved algorithm, this paper proposes a use GPS positioning information and prediction filter on vehicle dynamic model error estimation method.
9845 最后的半实物仿真实验结果表明,飞行器动力学信息辅助滤波器可以有效地减小系统误差,提高MEMS惯导系统输出精度。 ‭The last of the hardware-in-the-loop simulation experimental results show that the flight dynamics information support filter can effectively reduce the system error, improve the output precision MEMS inertial navigation system. ‭
9846 针对军事威胁的不确定性与模糊性和武器装备体系作战能力目标的抽象性,以任务需求为牵引,提出了一种面向任务的武器装备体系作战能力需求满足度分析方法。 Military threat against the uncertainty and fuzziness of abstractness and weapon equipment system operational capability goals, mission requirements for traction, this paper proposes a task-oriented operational capability of weapon equipment system demand satisfied degree analysis method.
9847 通过构建作战能力与作战任务质量屋,构建了面向任务的作战能力需求分析与指标权重计算模型; By building capabilities and combat mission of quality house, built a task oriented capability requirement analysis and the model of index weight;
9848 通过固有作战能力与作战能力需求的对比分析,提出了面向任务的作战能力需求满足度模型; Through the contrastive analysis of the inherent capability and combat capability requirements, puts forward the task oriented capability demand satisfaction model;
9849 进而提出了面向领域的多维度作战能力分析方法,实现了武器装备体系整体作战能力与领域作战能力的综合分析。 Then put forward the domain-oriented multidimensional operational capability analysis method, has realized the weapons and equipment system overall combat ability and capability in the field of comprehensive analysis.
9850 最后,以某地面突击装备体系作战能力分析为例,分析了该方法的可用性与有效性。 Finally, taking a ground assault equipment system operational capability analysis as an example, analyzes the availability and effectiveness of the method.
9851 以非对称伸缩翼飞行器为对象,构建了非对称变翼下的飞行器动力学模型,分析了非对称变翼对动力学的影响特性。 With asymmetric telescopic wing flight vehicle as the object, build the asymmetric change under the wing of vehicle dynamics model, analyzed the asymmetric variable wing's influence on the dynamic characteristics.
9852 首先,运用牛顿-欧拉法建立了飞行器多刚体动力学模型,突出了非对称伸缩变形所产生的模型差异;‭ ‭First of all, Newton - euler method is applied to build the aircraft rigid body dynamics model, highlighting the model produced by asymmetric expansion deformation difference;
9853 其次,以流体力学计算软件计算获得的气动数据为依据,探讨了非对称伸缩变形对飞行器质心偏移、转动惯量、气动特性、滚转力矩和纵向静稳定性的动力学特性的影响规律。 ‭Second, using fluid mechanics calculation on the basis of the aerodynamic data for calculation software, this paper discusses the asymmetric expansion deformation of the vehicle mass center offset, moment of inertia and aerodynamic characteristics, roll moment and the influence law of dynamic characteristics of the longitudinal static stability.