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911.
Hong Li Xiangyun Long Hua Feng Qiong Wu Jiahui Huang Weichun Jiang Massimo Minuti Dongxin Yang Saverio Citraro Hikmat Nasimi Jiandong Yu Ge Jin Ming Zeng Peng An Luca Baldini Ronaldo Bellazzini Alessandro Brez Luca Latronico Enrico Costa 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(1):708-714
PolarLight is a compact soft X-ray polarimeter onboard a CubeSat, which was launched into a low-Earth orbit on October 29, 2018. In March 2019, PolarLight started full operation, and since then, regular observations with the Crab nebula, Sco X-1, and background regions have been conducted. Here we report the operation, calibration, and performance of PolarLight in the orbit. Based on these, we discuss how one can run a low-cost, shared CubeSat for space astronomy, and how CubeSats can play a role in modern space astronomy for technical demonstration, science observations, and student training. 相似文献
912.
Jing Feng Binbin Ni Peng Lou Na Wei Longquan Yang Wen Liu Zhengyu Zhao Xue Li 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(10):2593-2608
HF sky-wave backscatter sounding system is capable of measuring the large-scale, two-dimensional (2-D) distributions of ionospheric electron density. The leading edge (LE) of a backscatter ionogram (BSI) is widely used for ionospheric inversion since it is hardly affected by any factors other than ionospheric electron density. Traditional BSI inversion methods have failed to distinguish LEs associated with different ionospheric layers, and simply utilize the minimum group path of each operating frequency, which generally corresponds to the LE associated with the F2 layer. Consequently, while the inversion results can provide accurate profiles of the F region below the F2 peak, the diagnostics may not be so effective for other ionospheric layers. In order to resolve this issue, we present a new BSI inversion method using LEs associated with different layers, which can further improve the accuracy of electron density distribution, especially the profile of the ionospheric layers below the F2 region. The efficiency of the algorithm is evaluated by computing the mean and the standard deviation of the differences between inverted parameter values and true values obtained from both vertical and oblique incidence sounding. Test results clearly manifest that the method we have developed outputs more accurate electron density profiles due to improvements to acquire the profiles of the layers below the F2 region. Our study can further improve the current BSI inversion methods on the reconstruction of 2-D electron density distribution in a vertical plane aligned with the direction of sounding. 相似文献
913.
Objective and accurate classification model or method of cloud image is a prerequisite for accurate weather monitoring and forecast. Thus safety of aircraft taking off and landing and air flight can be guaranteed. Thresholding is a kind of simple and effective method of cloud classification. It can realize automated ground-based cloud detection and cloudage observation. The existing segmentation methods based on fixed threshold and single threshold cannot achieve good segmentation effect. Thus it is difficult to obtain the accurate result of cloud detection and cloudage observation. In view of the above-mentioned problems, multi-thresholding methods of ground-based cloud based on exponential entropy/exponential gray entropy and uniform searching particle swarm optimization (UPSO) are proposed. Exponential entropy and exponential gray entropy make up for the defects of undefined value and zero value in Shannon entropy. In addition, exponential gray entropy reflects the relative uniformity of gray levels within the cloud cluster and background cluster. Cloud regions and background regions of different gray level ranges can be distinguished more precisely using the multi-thresholding strategy. In order to reduce computational complexity of original exhaustive algorithm for multi-threshold selection, the UPSO algorithm is adopted. It can find the optimal thresholds quickly and accurately. As a result, the real-time processing of segmentation of groundbased cloud image can be realized. The experimental results show that, in comparison with the existing groundbased cloud image segmentation methods and multi-thresholding method based on maximum Shannon entropy, the proposed methods can extract the boundary shape, textures and details feature of cloud more clearly. Therefore, the accuracies of cloudage detection and morphology classification for ground-based cloud are both improved. 相似文献
914.
915.
随着航空运输业竞争日益激烈,生存与发展成为航空公司的重要焦点。并购重组作为有效并相对快捷、节约成本的核心竞争力获取方式,以东航并购上航为例,对比并购前后航空公司绩效结果的变化,分析了航空企业并购行为是否增加效益、产生协同效应以及规模经济的实况。 相似文献
916.
917.
从冶金方面分析了T250与30CrMnSiA材料焊接工艺性。通过手工钨极氩弧焊焊接工艺研究试验,选择焊丝材料,确定材料焊接状态,制定了合理有效的焊接工艺规范和措施。采用光学金相显微镜、维氏硬度测试和力学性能检测等手段,对T250与30CrMnSiA异种材料焊接接头金相组织、力学性能和显微硬度等方面进行详细分析。结果表明,T250和30GrMnSiA异种材料具有良好的焊接性,填充HT250焊丝,采用热输入量较小的焊接电流进行焊接,接头强度与30GrMnSiA材料强度相当。 相似文献
918.
本文采用动力类比法对用于核爆炸测量的空气动压探头的动态响应进行了理论分析,并对探头的三个压力量程计算了总压边和静压边进气管道中的阻尼孔直径和动压波形的上升时间。分析计算表明,在探头的三个系统中,电学系统对动态响应的影响可忽略不计;力学系统的影响也是较小的;对动态响应起主要作用的是声学系统(即管道空腔系统)。在直径为130mm 激波管中进行了全尺寸探头的动态响应实验。实验表明,阻尼孔直径和波形上升时间的实验值与计算值符合较好。此探头曾多次用于我国大气层核试验测试中。从核爆炸和激波管实验中测得的空气动压波形可看出,它们的前沿都是很好的,这反映出此探头具有良好的动态响应特性。 相似文献
919.
Optimal guidance based on receding horizon control for low-thrust transfer to libration point orbits
Haijun Peng Qiang Gao Zhigang Wu Wanxie Zhong 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
This paper addresses the design and computation of a guidance law for a transfer mission from an orbit near the Earth to a halo orbit around the libration point L2 in the Sun–Earth system. The guidance law, which is designed based on receding horizon control and compensates for launch velocity errors that are introduced by inaccuracies of the launch vehicle, is solved using the generating function method. During the design of the closed-loop guidance law, the entire transfer mission, which is considered a nonlinear optimal control problem, is evaluated to obtain a nominal reference trajectory. Using the launch velocity errors and the uncertainty of the model, a spacecraft controlled by the proposed guidance law tracks the reference trajectory. Furthermore, the original Riccati differential equation in the receding horizon control algorithm is replaced by an equivalent convenient form of the Riccati differential equation that is based on the generating function. The high-efficiency solution of the equivalent equation avoids the online direct integration of the original Riccati differential equation, which significantly increases the computational efficiency for the receding horizon control problem. Numerical simulations using a nonlinear bicircular four-body model demonstrate the capabilities of the proposed receding horizon guidance law for the transfer mission. In addition, the generating function method improves the computational efficiency by at least one order of magnitude over the backward sweep method in solving the receding horizon control problem. 相似文献
920.
基于一类具有零扭转特性的并联机构原理并结合所设计的载荷解耦装置,设计了一种可对扭矩、弯矩、轴向力3种载荷进行复合模拟的负载模拟器;控制系统以可编程多轴运动控制器(PMAC,Programmable Multi-Axis motion Controller)为核心,通过力传感器测得的负载反馈值,采用力、位置、电流三闭环的控制策略,在有效避免系统电磁干扰噪声对传感器信号影响的同时,能够稳定地、较为准确地以正弦波的方式完成对扭矩、弯矩、轴向力等载荷的复合模拟.通过对静态加载对象复合负载模拟的现场试验,验证了本系统机构设计的合理性和控制策略的可行性. 相似文献