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Hybrid-Traffic-Detour Based Load Balancing for Onboard Routing in LEO Satellite Networks 被引量:12
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作者 Peilong Liu Hongyu Chen +2 位作者 Songjie Wei Limin Li zhencai zhu 《China Communications》 SCIE CSCD 2018年第6期28-41,共14页
To deal with the dynamic and imbalanced traffic requirements in Low Earth Orbit satellite networks, several distributed load balancing routing schemes have been proposed. However, because of the lack of global view, t... To deal with the dynamic and imbalanced traffic requirements in Low Earth Orbit satellite networks, several distributed load balancing routing schemes have been proposed. However, because of the lack of global view, these schemes may lead to cascading congestion in regions with high volume of traffic. To solve this problem, a Hybrid-Traffic-Detour based Load Balancing Routing(HLBR) scheme is proposed, where a Long-Distance Traffic Detour(LTD) method is devised and coordinates with distributed traffic detour method to perform self-adaptive load balancing. The forwarding path of LTD is acquired by the Circuitous Multipath Calculation(CMC) based on prior geographical information, and activated by the LTDShift-Trigger(LST) through real-time congestion perception. Simulation results show that the HLBR can mitigate cascading congestion and achieve efficient traffic distribution. 展开更多
关键词 satellite networks load balancing cascading congestion traffic detour
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Einstein Probe discovery of EP240408a:A peculiar X-ray transient with an intermediate timescale
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作者 Wenda Zhang Weimin Yuan +137 位作者 Zhixing Ling Yong Chen Nanda Rea Arne Rau Zhiming Cai Huaqing Cheng Francesco Coti Zelati Lixin Dai Jingwei Hu Shumei Jia Chichuan Jin Dongyue Li Paul O’Brien Rongfeng Shen Xinwen Shu Shengli Sun Xiaojin Sun Xiaofeng Wang Lei Yang Bing Zhang Chen Zhang Shuang-Nan Zhang Yonghe Zhang Jie An David Buckley Alexis Coleiro Bertrand Cordier Liming Dou Rob Eyles-Ferris Zhou Fan Hua Feng Shaoyu Fu Johan P.U.Fynbo Lluis Galbany Saurabh W.Jha Shuaiqing Jiang Albert Kong Erik Kuulkers Weihua Lei Wenxiong Li Bifang Liu Mingjun Liu Xing Liu Yuan Liu zhu Liu Chandreyee Maitra Alessio Marino Itumeleng Monageng Kirpal Nandra Jeremy Sanders Roberto Soria Lian Tao Junfeng Wang Song Wang Tinggui Wang Zhongxiang Wang Qingwen Wu Xuefeng Wu Dong Xu Yanjun Xu Suijian Xue Yongquan Xue Zijian Zhang Zipei zhu Hu Zou Congying Bao Fansheng Chen Houlei Chen Tianxiang Chen Wei Chen Yehai Chen Yifan Chen Chenzhou Cui Weiwei Cui Yanfeng Dai Dongwei Fan Ju Guan Dawei Han Dongjie Hou Haibo Hu Maohai Huang Jia Huo Zhenqing Jia Bowen Jiang Ge Jin Chengkui Li Junfei Li Longhui Li Maoshun Li Wei Li Zhengda Li Tianying Lian Congzhan Liu Heyang Liu Huaqiu Liu Fangjun Lu Laidan Luo Jia Ma Xuan Mao Haiwu Pan Xin Pan Liming Song Hui Sun Yunyin Tan Qingjun Tang Yihan Tao Hao Wang Juan Wang Lei Wang Wenxin Wang Yilong Wang Yusa Wang Qinyu Wu Haitao Xu Jingjing Xu Xinpeng Xu Yunfei Xu Zhao Xu Changbin Xue Yulong Xue Ailiang Yan Haonan Yang Xiongtao Yang Yanji Yang Juan Zhang Mo Zhang Wenjie Zhang Zhen Zhang Zhen Zhang Ziliang Zhang Donghua Zhao Haisheng Zhao Xiaofan Zhao Zijian Zhao Hongyan Zhou Yilin Zhou Yuxuan zhu zhencai zhu 《Science China(Physics,Mechanics & Astronomy)》 2025年第1期218-236,共19页
We report the discovery of a peculiar X-ray transient,EP240408a,by Einstein Probe(EP)and follow-up studies made with EP,Swift,NICER,GROND,ATCA and other ground-based multiwavelength telescopes.The new transient was fi... We report the discovery of a peculiar X-ray transient,EP240408a,by Einstein Probe(EP)and follow-up studies made with EP,Swift,NICER,GROND,ATCA and other ground-based multiwavelength telescopes.The new transient was first detected with Wide-field X-ray Telescope(WXT)on board EP on April 8th,2024,manifested in an intense yet brief X-ray flare lasting for 12 s.The flare reached a peak flux of 3:9×10^(−9) erg cm^(−2) s^(−1) in 0.5-4 keV,∼300 times brighter than the underlying X-ray emission detected throughout the observation.Rapid and more precise follow-up observations by EP/FXT,Swift and NICER confirmed the finding of this new transient.Its X-ray spectrum is non-thermal in 0.5-10 keV,with a power-law photon index varying within 1.8-2.5.The X-ray light curve shows a plateau lasting for∼4 d,followed by a steep decay till becoming undetectable∼10 d after the initial detection.Based on its temporal property and constraints from previous EP observations,an unusual timescale in the range of 7-23 d is found for EP240408a,which is intermediate between the commonly found fast and long-term transients.No counterparts have been found in optical and near-infrared,with the earliest observation at 17 h after the initial X-ray detection,suggestive of intrinsically weak emission in these bands.We demonstrate that the remarkable properties of EP240408a are inconsistent with any of the transient types known so far,by comparison with,in particular,jetted tidal disruption events,gamma-ray bursts,X-ray binaries and fast blue optical transients.The nature of EP240408a thus remains an enigma.We suggest that EP240408a may represent a new type of transients with intermediate timescales of the order of∼10 d.The detection and follow-ups of more of such objects are essential for revealing their origin. 展开更多
关键词 X-RAY transients Einstein Probe
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Friction and wear of multiple steel wires in a wire rope 被引量:4
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作者 Yuxing PENG Kun HUANG +5 位作者 Chenbo MA zhencai zhu Xiangdong CHANG Hao LU Qing ZHANG Chunming XU 《Friction》 SCIE EI CAS CSCD 2023年第5期763-784,共22页
The fretting wear among the steel wires aggravates the wire rope’s fatigue damage,affects the service performance of the wire ropes,and threatens mine hoisting safety.In this paper,the practical friction behavior and... The fretting wear among the steel wires aggravates the wire rope’s fatigue damage,affects the service performance of the wire ropes,and threatens mine hoisting safety.In this paper,the practical friction behavior and wear mechanism among the wires in the wire rope are investigated.A series of tests were carried out on multiple steel wires in helical contact and tension–torsion coupling under different fretting parameters,twisting parameters,and lubrication conditions by self-made friction and wear testing machine.The results show that the coefficient of friction(COF)among the steel wires decreases slightly with increasing lateral loads and tension,and the effect of twist angle on the COF has opposite results under different lubrication conditions.Lateral loads,tension of the steel wires,twist angle,and lubrication condition all affect the fretting morphology among the steel wires.Fretting wear with larger twist angle structure leads to more energy loss.The energy loss of fretting is directly related to the fretting morphology among the contact surfaces,and the dissipated energy is lower in the two forms of complete slip and sticking.The wear depth and width increase with the increase of lateral loads,steel wire tension,and twist angle.And the wear width and depth under dry friction conditions are higher than those under oil lubrication conditions.In addition,the wear mechanism under dry friction conditions is mainly abrasive wear,adhesive wear,and fatigue wear.And the wear mechanism under oil lubrication conditions is mainly abrasive wear and fatigue wear. 展开更多
关键词 steel wires fretting friction behavior helical contact wear mechanism
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Orbit Determination and Thrust Estimation for Noncooperative Target Using Angle-Only Measurement
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作者 Zhixun Zhang Leizheng Shu +4 位作者 Keke Zhang zhencai zhu Meijiang Zhou Xinwei Wang Weidong Yin 《Space(Science & Technology)》 EI 2023年第1期496-513,共18页
The classical interactive multimodel(IMM)algorithm has some disadvantages in tracking a noncooperative continuous thrust maneuvering spacecraft,such as poor steady-state accuracy,difficult selection of subfilter param... The classical interactive multimodel(IMM)algorithm has some disadvantages in tracking a noncooperative continuous thrust maneuvering spacecraft,such as poor steady-state accuracy,difficult selection of subfilter parameters,and mismatched model jump.To address the abovementioned problems,a variable-dimensional adaptive IMM strong tracking filtering algorithm(VAIMM-STEKF)is proposed to estimate the spacecraft’s position,velocity,and maneuvering acceleration state.VAIMM-STEKF contains 2 models,model 1 and model 2,which correspond to the tracking of the spacecraft in maneuvering and nonmaneuvering situations.Model 1 estimates the position and velocity of the spacecraft to ensure tracking accuracy when no maneuver occurs.Model 2 is a strong tracking filter with an augmented state.The adaptive IMM algorithm adjusts the fixed Markov transfer matrix in real time according to the model output probability.According to the different states of the spacecraft,the corresponding model interactive fusion method,together with the strong tracking filter,is adopted to ensure fast tracking when the spacecraft state changes.This method can also adapt to continuous thrust maneuvering spacecraft with different orders of magnitude.Simulation results show that the position accuracy of VAIMM-STEKF can be improved by approximately 27%and the speed accuracy can be enhanced by approximately 17%under different levels of maneuvering acceleration compared with those of the IMM algorithm.The convergence speed of VAIMM-STEKF is also better than the IMM algorithm. 展开更多
关键词 ACCELERATION INTERACTIVE ANGLE
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