An Improved Initial Orbit Determination Method Based on Perturbed Unit Vector Method
文献类型:期刊论文
作者 | Mao, YX; Ma, JY; Ni, XQ; Xiang, J |
刊名 | INTERNATIONAL CONFERENCE ON ELECTRICAL AND CONTROL ENGINEERING (ICECE 2015)
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出版日期 | 2015 |
期号 | 0页码:123-128 |
英文摘要 | We considered 18 solar flares observed between June 2010 and July 2012, in which high energy >100 MeV gamma-emission was registered by the Large Area Telescope (LAT) aboard FermiGRO. We exainined for these y-events soft X-ray observations by GOES, hard X-ray observations by the Anti-Coincidence Shield of the SPectrometer aboard INTEGRAL (ACS SPI) and the Gamma-Ray burst Monitor (GBM) aboard FemiGRO. Hard X-ray and mu-decay gamma-ray emissions are used as tracers of electron and proton acceleration, respectively. Bursts of hard X-ray were observed by ACS SPI during impulsive phase of 13 events. Bursts of hard X-ray >100 keV were not found during time intervals, when prolonged hard y-emission was registered by LAT/FermiGRO. Those events showing prolonged high-energy gamma-ray emission not accompanied by >100 keV hard X-ray emission arc interpreted as an indication of either different acceleration processes for protons and electrons or as the presence of a proton population accelerated during the impulsive phase of the flare and subsequently trapped by some magnetic structure. In-situ energetic particle measurements by GOES and STEREO (High Energy Telescope, HET) shows that five of these y-events were not accompanied by SEP events at 1 AU, even when multi-point measurements including STEREO are taken into account. Therefore accelerated protons are not always released into the heliosphere. A longer delay between the inaximum temperature and the maxiinum einission measure characterises flares with prolonged high energy gamma-emission and solar proton events. |
学科主题 | 天文和天体物理 |
收录类别 | SCI |
语种 | 英语 |
WOS记录号 | WOS:000361749700019 |
源URL | [http://libir.pmo.ac.cn/handle/332002/14922] ![]() |
专题 | 紫金山天文台_卫星精密定轨及应用研究团组 |
推荐引用方式 GB/T 7714 | Mao, YX,Ma, JY,Ni, XQ,et al. An Improved Initial Orbit Determination Method Based on Perturbed Unit Vector Method[J]. INTERNATIONAL CONFERENCE ON ELECTRICAL AND CONTROL ENGINEERING (ICECE 2015),2015(0):123-128. |
APA | Mao, YX,Ma, JY,Ni, XQ,&Xiang, J.(2015).An Improved Initial Orbit Determination Method Based on Perturbed Unit Vector Method.INTERNATIONAL CONFERENCE ON ELECTRICAL AND CONTROL ENGINEERING (ICECE 2015)(0),123-128. |
MLA | Mao, YX,et al."An Improved Initial Orbit Determination Method Based on Perturbed Unit Vector Method".INTERNATIONAL CONFERENCE ON ELECTRICAL AND CONTROL ENGINEERING (ICECE 2015) .0(2015):123-128. |
入库方式: OAI收割
来源:紫金山天文台
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