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701.
《中国航空学报》2023,36(5):157-174
The Secondary Air System (SAS) plays an important role in the safe operation and performance of aeroengines. The traditional 1D-3D coupling method loses information when used for secondary air systems, which affects the calculation accuracy. In this paper, a Cross-dimensional Data Transmission method (CDT) from 3D to 1D is proposed by introducing flow field uniformity into the data transmission. First, a uniformity index was established to quantify the flow field parameter distribution characteristics, and a uniformity index prediction model based on the locally weighted regression method (Lowess) was established to quickly obtain the flow field information. Then, an information selection criterion in 3D to 1D data transmission was established based on the Spearman rank correlation coefficient between the uniformity index and the accuracy of coupling calculation, and the calculation method was automatically determined according to the established criterion. Finally, a modified function was obtained by fitting the ratio of the 3D mass-average parameters to the analytical solution, which are then used to modify the selected parameters at the 1D-3D interface. Taking a typical disk cavity air system as an example, the results show that the calculation accuracy of the CDT method is greatly improved by a relative 53.88% compared with the traditional 1D-3D coupling method. Furthermore, the CDT method achieves a speedup of 2 to 3 orders of magnitude compared to the 3D calculation. 相似文献
702.
大气环境监测卫星是首颗生态环境领域大气环境监测专用卫星。卫星搭载了5台有效载荷,可实现CO2主动激光探测和大气细颗粒物的主被动结合探测,以及对气态污染物、云和气溶胶、水环境、自然生态等要素大范围、全天时综合监测,为生态环境遥感监管提供重要的数据支撑。本文从卫星载荷特点及数据获取能力出发,分析了其在生态环境行业的应用能力,并从大气环境、水环境和生态环境监测3个方面,结合在轨测试情况对卫星的应用能力进行详细阐述,可为开展大气环境监测卫星遥感应用提供参考。 相似文献
703.
针对城市环境下卫星导航系统用户接收终端对电文编译码算法的低复杂度和抗衰落性能需求,以北斗导航系统B-CNAV1电文为改进对象提出了一种外码采用RS码、内码采用二进制LDPC码的电文级联编码方法。通过RS码提高电文对抗突发错误的能力,同时利用二进制LDPC码保证电文对抗随机错误的能力。采用LMS信道对城市接收环境建模,仿真结果验证了本文提出的RS-LDPC级联码与B-CNAV1电文64进制LDPC码具有相近的性能,同时大幅降低了算法复杂度,较好地实现了电文纠错性能和实现复杂度的平衡,提供了一种适用于城市环境的高性能、低复杂度电文编码方法。 相似文献
704.
The main task of this work is to design a control system for a small tail-sitter Unmanned Aerial Vehicle(UAV) during the transition process. Although reasonable control performance can be obtained through a well-tuned single PID or cascade PID control architecture under nominal conditions, large or fast time-varying disturbances and a wide range of changes in the equilibrium point bring nonlinear characteristics to the transition control during the transition process, which leads to control prec... 相似文献
705.
随着5G通信和自动驾驶汽车的发展,车辆自组织网络VANET(Vehicular Ad Hoc Network)作为一种新型的移动自组织网络,因其在改善道路安全、为驾驶员和乘客提供便利方面的潜力,而引起学术界和工业界的广泛关注。它可以通过提供交通流量、事故通知、危险警告、可能存在的定位偏差、天气等信息来增强道路安全,从而提高交通效率。由于车辆的高速移动会经常引起网络拓扑中断,因此一个设计良好的路由协议至关重要。提出了一种适用于车辆自组织网络环境的基于分簇的路由协议,设计并实现了一种基于亲和传播算法的分簇组网模型V-APC(VANET-Affinity Propagation Clustering)。通过重新定义亲和传播算法的相似函数,设计了簇头的选择过程、簇的形成过程还有簇的维护过程。结果表明:采用上述方法形成的簇,在簇内的通信性能和簇稳定性方面具有显著优势,使得该协议在路由延迟和数据包转发成功率方面表现优异。 相似文献
706.
针对火星探测器着陆巡视器减速伞筒盖结构在轨运行耐温度交变、辐照等空间环境和再入过程耐温度冲击性能需求,重点开展了筒盖复合材料耐温匹配性、力学性能、耐空间环境性能以及制件成型工艺研究。结果表明,选用J-168-1胶黏剂、J-245胶黏剂及T300/QY8911复合材料制备的试件通过各项性能试验考核,均能满足筒盖结构的设计指标要求。筒盖产品力学性能稳定,成型工艺可行性良好,最高瞬时使用温度可达200℃,经历空间环境模拟后力学性能保持率均在80%以上,耐高温、耐空间环境性良好。产品已成功装星发射,并在着陆巡视器落火阶段成功弹出分离,圆满完成使命。 相似文献
707.
708.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2023,71(6):2702-2710
The European Stratospheric Balloon Observatory (ESBO) initiative aims at simplifying the access to stratospheric balloon missions. We plan to provide platforms and support with instrument design in order to support scientists. During the design process, the inevitable question of qualification for the harsh flight conditions arises. Unfortunately, there is no existing standard for qualification of stratospheric ballooning hardware. Thus, we developed a qualification procedure for use within ESBO and similar projects.In this paper, we present our analysis of the environmental conditions in the stratosphere. While conditions at typical balloon float altitudes are similar to the space environment, there are also some relevant differences. For example, the thermal environment is dominated by radiation and thermal conduction, but the remaining atmosphere still supports a certain amount of convection. The remaining atmospheric pressure in the stratosphere also leads to reduced arcing distances. Vibrational loads are far less than for space missions, but quasi-static or shock loads may occur. The criticality of radiation increases with mission duration.Based on the environmental conditions, we present the qualification procedures for ESBO, which are based on the European Cooperation for Space Standardization (ECSS) standards for space systems. Overtesting against too high requirements leads to overengineering, driving mission cost and mitigating the advantages of balloons over space missions. Therefore, we modified the ECSS standards to fit typical scientific ballooning missions over several days at altitudes up to 40 km. Furthermore, we analyzed design rules for space systems with regard to their relevance for scientific ballooning, including material and component selection. We present the experience from the hardware qualification process for the ESBO prototype STUDIO (Stratospheric UV Demonstrator of an Imaging Observatory). Even though boundary conditions are different for each individual mission, we aimed for a broader approach: We investigated more general requirements for scientific ballooning missions to support future flights. 相似文献
709.
710.