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301.
This paper presents an actuator used for the trajectory correction fuze, which is subject to high impact loadings during launch. A simulation method is carried out to obtain the peak-peak stress value of each component, from which the ball bearings are possible failures according to the results. Subsequently, three schemes against impact loadings, full-element deep groove ball bearing and integrated raceway, needle roller thrust bearing assembly, and gaskets are utilized for redesigning the actuator to effectively reduce the bearings' stress. However, multi-objectives optimization still needs to be conducted for the gaskets to decrease the stress value further to the yield stress. Four gasket's structure parameters and three bearings' peak-peak stress are served as the four optimization variables and three objectives, respectively. Optimized Latin hypercube design is used for generating sample points, and Kriging model selected according to estimation result can establish the relationship between the variables and objec-tives, representing the simulation which is time-consuming. Accordingly, two optimization algorithms work out the Pareto solutions, from which the best solutions are selected, and verified by the simulation to determine the gaskets optimized structure parameters. It can be concluded that the simulation and optimization method based on these components is effective and efficient. 相似文献
302.
In order to predict the storage life of a certain type of HTPB (hydroyl-terminated polybutadiene) coating at 25 C and analyze the influence of pre-strain on the storage life, the accelerated aging tests of HTPB coating at 40 C, 50 C, 60 C, 70 C with the pre-strain of 0%, 3%, 6%, 9%, respectively were carried out. The variation regularity of the change of crosslinking density was analyzed and the aging model of HTPB coating under pre-strained thermally-accelerated aging was proposed. The storage life of HTPB coating at 25 C was estimated by using the Berthelot equation as the end point of the aging life with a 30% decrease in maximum elongation. The results showed that the change of crosslinking density of HTPB coating increased with the increase of aging temperature and aging time, and decreased with the in-crease of pre-strain. Under 0% pre-strain, the relationship between the change of crosslinking density of HTPB coating and the aging time can be described by the logarithmic model with the confidence probability greater than 99%.The stress relaxation phenomenon existed under 3%, 6% and 9% pre-strained aging. The aging model considering chemical aging and pre-strain was established with the confidence probability greater than 90%. The storage life of HTPB coating was 15.2935 years at 25 C under 0% pre-strain, which was reduced by 13.9007%, 75.6949% and 89.7859% under 3%, 6% and 9% pre-strain, respectively. The existence of pre-strain has a serious impact on the storage life of HTPB coating, therefore, the pre-strain should be avoided as much as possible during the actual storage. 相似文献
303.
描述了路面不平度的统计特性,建立了AR模型。运用现代谱估计的方法对沙土地、硬土地和耕地等非人工路面的频谱特性进行了分析,得到了沙土地等3种路面的加速度功率谱和位移功率谱密度曲线图。结果表明,沙土地和耕地路面要好于硬土地路面,该结论与常识相符,验证了用AR模型法进行功率谱分析的可靠性和可行性。 相似文献
304.
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306.
基于离散降雨衰耗状态的卫星信道模型 总被引:1,自引:0,他引:1
针对Ka频段卫星信道中降雨衰耗的统计分布特点,建立了基于离散降雨衰耗状态的卫星信道模型,模型中各状态组成离散的Markov链并由其转移概率矩阵来表示,分析此模型下的信道误比特性能和数据包丢失性能。此模型能够适用于链路层以及高层通信协议。 相似文献
307.
为解决快速实时的在线状态监控与决策这一与系统功能相适应的问题,针对FMS加工设备与过程的特点和对之进行监控与诊断的需要,提出一通用的全局监测与决策模型,包括传感策略、特征提取、状态表述与分类、故障全局综合决策等模块和具体的监测流程。 相似文献
308.
309.
根据导弹作战机动过程各路段机动时间随机性特点,运用随机规划理论建立了导弹机动任务规划的数学模型,设计了遗传算法求解策略,实现了在一定时间内合理地规划机动路线的任务,并通过算例作了说明。该方法可用于导弹机动路径选择,为导弹作战机动计划的制定提供决策依据。 相似文献
310.
由于粒子滤波的算法原理,其计算量很大。研究了针对机动目标的交互式多模型粒子滤波器(IMMPF)算法和多速率交互式多模型(MRIMM)算法,提出了多速率交互式多模型粒子滤波器(MRIMMPF)算法。该算法是在交互式多模型粒子滤波器(IMMPF)的基础上引入多速率技术,期望在保持IMMPF的性能同时能够减少因为粒子滤波带来的计算量;最后通过和一般基于EKF的IMM算法、IMMPF算法的比较,验证了该算法的有效性。 相似文献