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针对3种不同相变温度的相变材料组成的组合吸热器,建立了相应的物理模型,给出了数值求解方法,计算了工质入口温度、工质流速及输入功率等操作参数对组合式吸热器热性能的影响,得到了容器壁面最高温度、工质出口温度、换热管总相变蓄热材料(PCM)熔化率等结果.结果表明操作参数对吸热器热性能有较大的影响,合理选取这些参数对吸热器的正常运行是非常必要的,结果可以用于指导吸热器的设计. 相似文献
334.
神经外科手术机器人灵活性分析 总被引:16,自引:2,他引:14
开发了用于神经外科手术的五自由度机器人BH600.从神经外科立体定向手术的需求出发,分析了该机器人的灵活性.用服务球和服务区概念给出了五自由度机器人工作空间任意点的灵活度定义,提出了工作空间灵活性的分析方法.通过数值计算和图形显示给出了工作空间的灵活度分布,采用机器人物理样机进行实验,对分析结果进行了验证.掌握灵活度的空间分布,可以为手术路径规划提供可靠的依据. 相似文献
335.
GALILEO接收机中BOC(1,1)信号的捕获 总被引:10,自引:0,他引:10
BOC(1,1)(Binary-Offset-Carrier)信号相关函数中的零值会使接收机判定没有捕获到信号.为了完全捕获到BOC(1,1)信号,从副载波相位和码相位角度出发,提出了一种3路并行捕获方法.通过数字仿真得到了BOC(1,1)和扩频码的相关函数图,比较了二者相关函数的峰值.推导了BOC(1,1)相关函数的解析式,给出了相关函数中的零点位置和峰值位置,比较了BOC(1,1)和扩频码的相关函数数值及捕获.3路本地BOC信号以其中一路相位为基准,另外2路相位分别超前、滞后该路.给出了3路本地信号的生成方法及捕获的结构框图.仿真结果表明,捕获码相位差在半个码片内时,BOC(1,1)信号的捕获率从33.3%提高到100%,码相位捕获范围从1/6码片增大到1/2码片.该方法可为跟踪环路提供相位信息,适用于BOC(n,n)信号的捕获. 相似文献
336.
This article presents a novel electrical/mechanical hybrid 4-redundancy brushless DC torque motor (BLDCM), which has found applications in direct drive actuators (DDA) of aerial vehicles. This motor is characteristic of electrical/mechanical hybrid 4-redundancy by securing two stators along with two rotors on the same shaft. Each stator contains two sets of windings embedded in separated slots. Furthermore, compared to the scheme of two electrical dual-redundancy BLDCMs linked by a mechanical transmission, the proposed motor has lower volume and lighter weight, eliminates the nonlinearity caused by the gap of the mechanical transmission, moderates the requirement for the torque balance between redundancies and reduces the cogging torque by shifting the magnets. Both magnetic circuit calculation and the finite element analysis (FEA) of the electromagnetic field are conducted to optimize the design process. A prototype motor has been produced and tested. The results indicate that its performances comply with the requirements presented by designers. Moreover, the position frequency response of the prototype in the DDA's unloaded situation has also demonstrated the fulfillment of desired dynamic characteristics. 相似文献
337.
Qing Zhao Wang Gao Chengfa Gao Shuguo Pan Xing Yang Jun Wang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(3):1124-1142
The main challenge in real-time precise point positioning (PPP) is that the data outages or large time lags in receiving precise orbit and clock corrections greatly degrade the continuity and real-time performance of PPP positioning. To solve this problem, instead of directly predicting orbit and clock corrections in previous researches, this paper presents an alternative approach of generating combined corrections including orbit error, satellite clock and receiver-related error with broadcast ephemeris. Using ambiguities and satellite fractional-cycle biases (FCBs) of previous epoch and the short-term predicted tropospheric delay through linear extrapolation model (LEM), combined corrections at current epoch are retrieved and weighted with multiple reference stations, and further broadcast to user for continuous enhanced positioning during outages of orbit and clock corrections. To validate the proposed method, two reference station network with different inter-station distance from National Geodetic Survey (NGS) network are used for experiments with six different time lags (i.e., 5 s, 10 s, 15 s, 30 s, 45 s and 60 s), and one set of data collected by unmanned aerial vehicle (UAV) is also used. The performance of LEM is investigated, and the troposphere prediction accuracy of low elevation (e.g., 10–20degrees) satellites has been improved by 44.1% to 79.0%. The average accuracy of combined corrections before and after LEM is used is improved by 12.5% to 77.3%. Without LEM, an accuracy of 2–3 cm can be maintained only in case of small time lags, while the accuracies with LEM are all better than 2 cm in case of different time lags. The performance of simulated kinematic PPP at user end is assessed in terms of positioning accuracy and epoch fix rate. In case of different time lags, after LEM is used, the average accuracy in horizontal direction is better than 3 cm, and the accuracy in up direction is better than 5 cm. At the same time, the epoch fix rate has also increased to varying degrees. The results of the UAV data show that in real kinematic environment, the proposed method can still maintain a positioning accuracy of several centimeters in case of 20 s time lag. 相似文献
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将高超声速飞行器双重不确定性因素建模为未知干扰输入项,针对状态演化方程和量测方程含有不同未知干扰输入的高超声速飞行器控制系统状态估计问题开展研究,提出一种基于自适应方差极小化的递推状态估计器(Adaptive variance minimization based Recursive Estimator, AVMRE)。首先建立了状态估计递推滤波器模型,实现滤波误差中的量测未知干扰解耦,之后引入自适应调整因子刻画状态未知干扰并推导了最小上界估计误差协方差矩阵,最后,基于最小方差估计准则设计了滤波器中的量测增益反馈矩阵。以外部突风和传感器故障为例,受内外部双重不确定性因素影响下的高超声速飞行器仿真实验验证了本文算法的有效性,与相关算法的仿真对比反映了本文算法的优越性。 相似文献