ID 原文 译文
6634 仿真对比结果表明:在追踪器控制量占优势的情况下,提出的最优控制策略可以使追踪器绕开防御器并且捕获逃逸器; Contrast the simulation results show that the tracking control of the dominant situation, put forward the optimal control strategy can make the tracker to bypass defense apparatus and capture the escape;
6635 在追踪器控制量不占优势的情况下,提出的最优控制策略可以延长追踪器被防御器拦截的时间。 In tracking control is the dominant situation, put forward the optimal control strategy can prolong the time of tracking blocked by defensive unit.
6636 皮纳卫星具有研制周期短、采用商用货架式器件的特点,无法完整沿用传统大卫星通过底层元器件或部组件搭建系统可靠性模型计算整星可靠性的方法。 , the satellite has a short development cycle, the characteristics of the device adopts the commercial shelves, unable to complete the traditional large satellite components set up by the underlying components or department system reliability calculation model of the reliability of the whole star method.
6637 针对上述问题,提出了基于试验数据的皮纳卫星可靠性评估体系。 According to the above problem, was proposed based on the test data, satellite reliability evaluation system.
6638 通过对机理不同的硬件和软件故障分别建模的方法,实现了ZDPS-2卫星的可靠性评估。 Through the mechanism of different hardware and software failure modeling method respectively, implements the ZDPS - 2 satellite reliability evaluation.
6639 对卫星的硬件故障数,基于顺序约束模型和贝叶斯参数估计方法进行拟合,并考虑了不同试验环境对卫星工作环境的等效因子。 Hardware failure number of satellite based on sequence constraint model and bayesian parameter estimation method for fitting, and considering the different test environment on the equivalent factor of the satellite working environment.
6640 ZDPS-2卫星硬件可靠性水平估计为3月末0.85。 ZDPS - 2 satellite hardware reliability estimates for the end of March 0.85.
6641 对卫星的软件故障采用加入变点的非齐次泊松过程模型拟合,并选择Logistic模型作为测试覆盖率模型。 Software of satellite fault by using variable point of nonhomogeneous poisson process model fitting, and select the Logistic model as the test coverage model.
6642 ZDPS-2卫星软件故障拟合结果,平均无故障时间为217h。 Software failure fitting results ZDPS - 2 satellite, MTBF for 217 h.
6643 ZDPS-2卫星试验结果证实,可靠性满足增长试验设计的要求和任务需求。 ZDPS - 2 satellite test results confirmed that meet the reliability growth test design requirements and task requirements.