ID 原文 译文
8194 在已有研究的基础上,研究了多旋翼飞行器在惯性积不可忽略时的可控性分析方法。 On the basis of existing research, we studied many rotor aircraft cannot be ignored in the inertial deposition of controllability analysis method.
8195 进一步地,提出了一种新的多旋翼飞行器可控性度量指标。 Further, this paper proposes a new rotor aircraft controllability metrics.
8196 与文献中已有指标相比,本文所提的指标不仅具有已有指标的功能,而且还能够反应飞行器惯性积的改变对其可控度的影响。 Compared with the existing in the literature index, index proposed in this paper not only has the function of existing index but also able to response the change of aircraft product of inertia on its controllable degree.
8197 最后,仿真结果表明了所给出的可控性分析方法以及可控性度量指标的有效性。 Finally, the simulation results show that the given control analysis method and the effectiveness of control measures.
8198 针对大型复杂装备维修力量的调度与分配复杂性,引入修理工多重休假策略,以包含n个相同部件的并联系统为研究对象。 For large complex equipment maintenance scheduling of power and complexity of distribution, introduced the repairman multiple vacation policy, to contain the same n parts of paralleling system as the research object.
8199 针对以往研究利用指数分布等典型分布导致模型约束条件过于严格的问题,假设系统部件寿命、维修时间以及修理工休假时间均服从连续Phase-type分布,建立了适用性更好的系统可靠性解析模型。 According to previous research using the index distribution of typical distribution lead to overly strict model constraint condition, assumes that the system life, repair time and repairman vacation time are subject to continuous Phase -type distribution, better applicability of system reliability analysis model is established.
8200 得到了系统可靠度、系统稳态可用度、稳态故障频度、系统平均故障间隔时间等一系列可靠性参数的解析表达式,并利用算例验证了模型适用性。 The system reliability, system steady-state availability, the steady-state fault frequency, MTBF and a series of system reliability parameters of analytical expression, the applicability and use numerical examples to verify the model.
8201 以故障拓展模型和概率检验模型为基础,通过分析概率检验模型的语法语义、转移命令及逻辑关系,研究清晰、完整的转换规则,实现故障拓展模型向概率检验模型的转换。 On the basis of fault development model and probability test model, through the analysis of the grammar semantics of probability test model, transfer orders and the logic relationship, study clear, complete transformation rules, probability of fault development model to test model transformation.
8202 此外,研究模型的定量概率检验转换规则,构建逻辑验证表达。 In addition, the quantitative probability test of the model transformation rules, construct validation logic expression.
8203 最后,对机载通信系统调谐控制功能展开基于概率检验的定量安全性评估。 Finally, based on the probability of airborne communication system tuning control function carried out by inspection of the quantitative safety assessment.