ID 原文 译文
11654 分别从作战使命层次和作战任务层次设计了指控效率、同步效率和负载率作为其效能测度指标。 ‭Respectively from the combat mission design and operations levels the charge efficiency, synchronization, efficiency and load factor as a performance measure.
11655 然后从结构高效性和鲁棒性的角度探讨了测度指标的选择对衡量C2组织信息结构效能的影响。 ‭Then from the Angle of structural efficiency and robustness, discusses the measure of choice to measure the effect of C2 organization structure of information efficiency.
11656 最后,基于加权积模型提出了一种C2组织信息结构效能综合评估方法,并通过一个案例证明了该方法的有效性和稳定性。 ‭Finally, based on the weighted product model puts forward a structure of C2 organization information performance comprehensive evaluation method, and through a case study to prove the effectiveness and stability of the method. ‭
11657 针对连续时空马尔可夫运动目标的最优搜索者路径问题(optimal searcher path problem,OSPP),建立了搜索者方向和速度均作为决策变量的搜索路径规划模型,给出了一种改进的双链遗传算法(improved double chains genetic algorithm,IDCGA)。 In view of the continuous time markov moving targets of the optimal search path problem (optimal a searcher path problem, OSPP), established the search direction and the speed as the decision variables of the search path planning model, presents a genetic algorithm is an improved double chain (improved double chains based algorithm, IDCGA).
11658 算法采用双链实数编码策略表达搜索路径,利用混沌初始化方法产生初始种群,提出了变异幅度自适应控制的方法。 Real number coding algorithm adopts double chain strategy to express the search path, using chaos initialization method to produce the initial population, the variability in adaptive control method.
11659 通过引入基因位自适应因子η和进化代数自适应因子λ对变异操作进行了改进。 An adaptive factor by introducing genes eta and evolution algebra adaptive factor lambda to mutation operation is improved.
11660 以反潜搜索问题为例进行的仿真实验表明,所提出的算法具有稳定性好、寻优能力强、收敛速度快等优点,适用于求解复杂搜索路径问题。 In antisubmarine search problems, for example of simulation experiment show that the proposed algorithm has good stability, strong optimization ability and fast convergence speed, is suitable for solving complex search path problem.
11661 基于气浮球轴承的航天器模拟器广泛用于研究航天器的姿态动力学与控制,为了在地面模拟太空中的失重环境,必须将重力力矩的干扰减到最小。 Spacecraft simulator based on gas floating ball bearing is widely used in the research of the spacecraft attitude dynamics and control, in order to simulate weightlessness in space on the ground, gravity torque must be to minimize the interference.
11662 因此,模拟器的旋转中心要与气浮球轴承的中心重合。 ‭As a result, the rotation of the simulator center to the floating ball bearing.
11663 提出一种自动配平系统的设计方法,将姿态稳定控制作为系统的内回路,自动配平作为系统的外回路。 ‭In this paper, a design method of the automatic balancing system, attitude stability control as a system of the circuits inside, automatic balancing as the outer loop of the system.