| ID | 原文 | 译文 |
| 8044 | 针对这一问题,从用户的角度着手,基于用户行为对云资源调度问题进行深入的研究,提出了基于用户行为反馈的资源调度机制(user behavior-based resource scheduling mechanism with feedback control,UBRSM-FC)。 | In order to solve this problem, from the perspective of users, based on user behavior to deeply research the cloud resource scheduling problem, based on user behavior feedback mechanism of resource scheduling (user behaviors - -based resource scheduling mechanism with feedback control, UBRSM - FC). |
| 8045 | UBRSM-FC利用用户交互行为,将用户行为信息融入到资源调度过程中,并结合相关反馈机制,建立用户需求的主动发现网络和反馈网络对调度过程不断微调和优化,使资源调度的结果与用户的主观感知更加接近。 | UBRSM - FC using user interaction, the user behavior in the process of information into the resource scheduling, and connecting with the relevance feedback mechanism, establish user needs take the initiative to find and feedback network constantly fine-tune the process of scheduling and optimization, the result of the resource scheduling with the user's subjective perception even closer. |
| 8046 | 实验结果表明,UBRSM-FC通过反馈控制能够更好地满足不同用户不同程度的资源请求,提高了用户满意度,而且能够兼顾系统资源的利用率。 | The experimental results show that the UBRSM - FC via feedback control can better satisfy different users different degree of resource request, improve customer satisfaction, and can give attention to both the utilization of system resources. |
| 8047 | 四旋翼飞行器为欠驱动形式,其模型存在强耦合、大不确定性的特征,需设计具有强抗扰和强鲁棒能力的控制器以提升四旋翼飞行性能。 | Four rotor aircraft for underactuated form, the model has characteristics of strong coupling and uncertainty, the need to design has a strong ability to resist interference and the strong robustness of the controller to enhance the four rotor flight performance. |
| 8048 | 首先建立包含结构参数不确定性的四旋翼飞行器动力学模型,分析其特性并基于时标分离原则进行模型的双回路划分。 | First establish contains four rotor aircraft dynamic model of structural parameter uncertainty, to analyze its characteristics and model based on the time-scale separation principle of double circuit partitioning. |
| 8049 | 利用小角度假设对模型进行线性化处理并求取模型的状态空间表达形式,给出满足不确定性区间内稳定控制要求的鲁棒控制律,并采用Lyapunov理论进行控制律的全局收敛性证明。 | Using small Angle assumption for linearization model and calculating model of state space form of expression, satisfy the requirement of uncertainty interval stability control is given, the robust control law and control law by using Lyapunov theory of the global convergence is proved. |
| 8050 | 为增强控制器的抗扰性,利用Super-twisting算法设计了滑模干扰观测器对外部扰动进行观测并予以补偿。 | For the perturbation resistance of enhanced controller, using the sliding mode disturbance observer was designed by the Super - twisting algorithm to external disturbance were observed and compensated. |
| 8051 | 仿真结果表明,所设计的基于滑模观测补偿的鲁棒动态逆控制器在应对较大结构不确定性和外部扰动情况具有良好的控制品质。 | The simulation results show that the designed robust dynamic inversion controller based on sliding mode observation compensation in dealing with the larger structure uncertainty and external disturbance situation has good control quality. |
| 8052 | 针对双基地多输入多输出(multiple input multiple output,MIMO)雷达目标角度跟踪问题,提出了一种改进型紧缩投影近似子空间跟踪(projection approximation subspace tracking deflation,PASTd)算法。 | For double base multiple input multiple output (multiple input multiple output, MIMO) Angle of radar target tracking problem, this paper proposes a modified austerity projection approximation subspace tracking (the projection approximation subspace tracking deflation, PASTd) is proposed. |
| 8053 | PASTd算法性能较好,被大量应用于双基地MIMO雷达角度跟踪中,但是PASTd算法不能跟踪相同发射角(direction of departure,DOD)或接收角(direction of arrival,DOA)的目标,并且无法实现不同时刻同一目标角度的自动关联。 | PASTd algorithm has good performance and is widely used in bistatic MIMO radar Angle tracking, but PASTd algorithm cannot follow the same emission Angle (direction of departure, DOD) or receiving Angle (DOA) direction of concatenated, goals, and cannot achieve the same target Angle different time automatically. |