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461.
用基于工业铂电阻的高精度数字温度计替代标准水银温度计,是当今温度计量的一个研究热点。迄今为止这类产品只能作为工作器具使用,其主要原因是对高精度数字温度计的长期稳定性研究还不充分。介绍了一款高精度数字温度计长达8年的稳定性研究成果,并和标准水银温度计比较,说明用高精度数字温度计替代标准水银温度计是完全可行的观点,同时提出一些具体建议。  相似文献   
462.
《中国航空学报》2023,36(8):148-167
Aircraft collaboration design is based on a unified set of schemas containing data and model representations and interfaces across disciplines. The aircraft design schema is a central data model that specifies the paradigm for the representation of a full lifecycle model of aircraft design. The construction of the schema currently lacks theoretical guidance. This paper designs a novel methodology to construct the aircraft design schema, a fully functional, logical, and self-consistent methodology. The methodology defines a schema matrix that includes implementation strategies, principles, processes, meta-object facility, views, scenarios, and products. The aircraft conceptual design schema is constructed according to the methodology, which is a hands-on approach to help understand the concept and implementation. The features of the methodology are analyzed, and the methodology and the aircraft conceptual design schema are presented to address the pain points of multiple solution trade-offs, multiple iterations, and multidisciplinary coupling in aircraft conceptual collaboration design.  相似文献   
463.
针对以引力波探测为代表的空间科学任务和以“国网星座计划”为代表的商用卫星网络任务对推进器的特殊需求,本文提出了一种基于数字孪生的推进器优化设计方法。该方法首先建立由机理模型模块和测试数据集模块组成的数字孪生体。机理模型模块依据推进器的物理过程建立模型,对难以测量的数据进行仿真模拟;测试数据集模块通过实验对推进器进行测试,依靠测试数据建立可测参数的数学模型。将数字孪生体与实验进行对比,通过对比结果反馈调节机理模块从而不断提高孪生体的准确性,最终为优化设计提供依据。结果表明:(1)该方法能够构建微波离子推进器的数字孪生体;(2)该数字孪生体的预测结果存在一定差异,通过分析发现该差异与机理模型的精细度以及测试数据集的数据量有关。  相似文献   
464.
《中国航空学报》2023,36(3):449-470
The digital twin-driven performance model provides an attractive option for the warn gas-path faults of the gas turbines. However, three technical difficulties need to be solved: (1) low modeling precision caused by individual differences between gas turbines, (2) poor solution efficiency due to excessive iterations, and (3) the false alarm and missing alarm brought by the traditional fixed threshold method. This paper proposes a digital twin model-based early warning method for gas-path faults that breaks through the above obstacles from three aspects. Firstly, a novel performance modeling strategy is proposed to make the simulation effect close to the actual gas turbine by fusing the mechanism model and measurement data. Secondly, the idea of controlling the relative accuracy of model parameters is developed. The introduction of an error module to the existing model can greatly shorten the modeling cycle. The third solution focuses on the early warning based on the digital twin model, which self-learns the alarm threshold of the warning feature of gas-path parameters using the kernel density estimation. The proposed method is utilized to analyze actual measured data of LM2500 +, and the results verify that the new-built digital model has higher accuracy and better efficiency. The comparisons show that the proposed method shows evident superiority in early warning of performance faults for gas turbines over other methods.  相似文献   
465.
为丰富和完善国家时间频率体系建设,提高现有定位导航与授时(PNT)体系的服务能力,中国科学院国家授时中心开展了基于数字卫星电视信号的授时方法研究,并搭建了一套数字卫星电视授时系统,实际测试结果表明其定时精度优于50ns(均方根).首先综述了数字卫星电视授时方法中的理论框架及其若干关键技术问题,然后介绍了在提高授时精度方面的研究进展,最后指出了数字卫星电视授时方法的应用场景和由此方法衍生出的电视卫星测定轨、目标定位等应用前景,并展望了未来的研究方向.  相似文献   
466.
《中国航空学报》2023,36(5):187-201
The adaptive feedback control of stability with circumferential inlet distortion has been experimentally investigated in a low-speed, axial compressor. The flat-baffles with different span heights are used to simulate different distorted inflow cases. Compared with auto-correlation and root-mean-square analysis, cross-correlation analysis used to predict early stall warning does not depend on the distortion position. Hence, the cross-correlation coefficient was used to monitor the stable status of the compressor and provide the feedback signal in the active control strategy when suffering from different distortions. Based on the stall margin improvement of tip air injection obtained under different distorted inflow cases and the sensitivity analysis of cross-correlation coefficients to injected momentum ratios, tip air injection was adopted as the actuator for adaptive feedback control. The digital signal processing controller was designed and applied to achieve adaptive feedback control in distorted inflow conditions. The results show that the adaptive feedback control of air injection nearly achieves the same stall margin improvement as steady air injection under different distortion intensities with a reduced injection mass flow. Thus, the proposed adaptive feedback control method is ideal for the engine operation with circumferential distorted inflow, which frequently occurs in flight.  相似文献   
467.
瞿伟哲 《遥测遥控》2023,44(1):57-63
基于PSK调制的数字通信系统在无线通信工程实践中有着广泛的应用,由于受到各种条件的限制,从实际工程系统接收到的PSK数字通信信号在教学科研中不易获得,而PSK调制仿真数据则可以自己产生。在掌握通信原理和仿真技术的基础上利用Matlab实现对BPSK、DPSK、QPSK、DQPSK、8PSK、π/4-DQPSK、OQPSK等数字通信信号源的模拟仿真,可对调制体制、工作频率、传输码率、采样频率、信道特征等参数进行灵活设置,并按要求生成规定格式的DAT数据文件,可作为调制方式识别软件的训练和测试样本。结合模方谱、平方谱、四次方谱、八次方谱等谱线参数特征,同时结合星座图和眼图进行基于PSK调制的数字通信信号的调制体制判别和验证。  相似文献   
468.
The force-generation mechanism of a dovelike flapping-wing micro air vehicle was studied by numerical simulation and experiment. To obtain the real deformation pattern of the flapping wing, the digital image correlation technology was used to measure the dynamic deformation of the wing. The dynamic deformation data were subsequently interpolated and embedded into the CFD solver to account for the aeroelastic effects. The dynamic deformation data were further used to calculate the inertial forces...  相似文献   
469.
In radiation detector signal processing, usually, the charge-sensitive preamplifier converts the small charge signal coming from the semiconductor-based detector into voltage form and then the signal is further amplified to measure the energy of the incoming radiation. The voltage pulse from a charge-sensitive preamplifier (CSPA) is amplified using a shaping amplifier which reduces the signal bandwidth. To achieve better energy resolution, precise measurement of the peak amplitude of shaping amplifier output is required. The signal processing methods are available in which the signal from the charge-sensitive preamplifier can be directly digitized using high-speed Analog to Digital Converters (ADC), and then further signal processing such as gain and shaping is carried out inside the Field Programmable Gate Arrays (FPGA). For multiple detector systems, digital signal processing methods are quite difficult to implement in Field Programmable Gate Arrays (FPGA). In this context, The development of an alternative technique is initiated that uses a charge-sensitive preamplifier, shaping amplifier, low sampling analog-to-digital converter, and FPGA, where LaGrange’s interpolation technique is implemented in FPGA to precisely measure the peak of the analog pulse. In this paper, the comparison of the proposed method with other pulse amplitude measurement techniques is discussed. Results show that the implemented technique gives similar energy resolution compared to digital pulse processing and standard peak detector-based techniques.  相似文献   
470.
从无人操控天线需要依赖数引完成目标自动捕获以及现有的主动段航天测量的数引模型精度不够的背景出发,指出提高数引精度即进行数引改进的必要性。然后结合末段跟踪的特殊性,从时差、视差和延时累积误差三个影响数引精度的最主要方面详细分析了它们的形成机理,并给出了各自的改进方法。  相似文献   
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