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301.
S.J. Wang D. Maia M. Pick G. Aulanier J.-M. Malherbe J.-P. Delaboudinire 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2005,36(12):2273
We present our research on a fast and decelerating partial halo coronal mass ejection (CME) event detected in multi-wavelengths in the chromosphere and the corona on 14 October, 1999. The event involved a whole complex active area which spanned more than 40° of heliolongitude. It included a strong solar flare (XI/1N) and a complex eruptive filament within an active region of the entire complex. Especially, several radio sources were detected in the decimetric range prior to the CME by the Nançay Radioheliograph (NRH). A linear force-free field extrapolation of the Michelson Doppler Imager (MDI) magnetogram was performed to calculate the magnetic topology of the complex prior to the triggering of the event. The presence of a coronal null point combined with the occurrence of two distant and nearly simultaneous radio sources put strong arguments in favor of the generalized breakout model for the triggering of the eruption. The analysis of the subsequent development of the event suggests that large interconnecting loops were ejected together with the CME. 相似文献
302.
Iain Moore Matteo Ceriotti 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(9):3027-3044
A major cause of spacecraft orbital variation comes from natural perturbations, which, in close proximity of a body, are dominated by its non-spherical nature. For small bodies, such as asteroids, these effects can be considerable, given their uneven (and uncertain) mass distribution. Solar sail technology is proposed to reduce or eliminate the net secular effects of the irregular gravity field on the orbit. Initially, a sensitivity analysis will be carried out on the system which will show high sensitivity to changes in initial conditions. This presents a challenge for optimisation methods which require an initial guess of the solution. As such, the Genetic Algorithm (GA) is proposed as the preferred optimisation method as this requires no initial guess from the user. A multi-objective optimisation is performed which aims to achieve a periodic orbit whilst also minimising the effort required by the sail to do so. Given the system sensitivity, the control law for one orbit is not necessarily applicable for any subsequent orbit. Therefore, a new method of updating the control law for subsequent orbits is presented, based on linearisation and use of a Control Transition Matrix (CTM). The techniques will later find application in a multiple asteroid rendezvous mission with a solar sail as the primary propulsion system. 相似文献
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在结构光视觉检测系统中,光条中心的提取精度直接影响到整个测量系统的测量精度.光条图像的处理是其中重要的一步,尤其是受到严重噪声干扰的图像.探讨了被多种噪声干扰的光条图像的处理和精确提取光条中心的方法.给出了一种消除环境干扰的滤波模板并实验验证了其滤波效果.使用这些光条图像处理方法使整个测量系统在200mm×200mm的测量范围内测量精度达到0.083mm. 相似文献
306.
Merlin C. Köhnke Christian von Savigny Charles E. Robert 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(10):2531-2539
Previous studies have identified solar 27-day signatures in several parameters in the Mesosphere/Lower thermosphere region, including temperature and Noctilucent cloud (NLC) occurrence frequency. In this study we report on a solar 27-day signature in NLC altitude with peak-to-peak variations of about 400?m. We use SCIAMACHY limb-scatter observations from 2002 to 2012 to detect NLCs. The superposed epoch analysis method is applied to extract solar 27-day signatures. A 27-day signature in NLC altitude can be identified in both hemispheres in the SCIAMACHY dataset, but the signature is more pronounced in the northern hemisphere. The solar signature in NLC altitude is found to be in phase with solar activity and temperature for latitudes N. We provide a qualitative explanation for the positive correlation between solar activity and NLC altitude based on published model simulations. 相似文献
307.
Hyper-thin, high-speed solar-photon sail space probes exploring the Sun?s Oort comet cloud could also be used to set an upper bound to the concentration of WIMPS (weakly interacting massive particles), one of the suggested (but unconfirmed) forms of dark matter within the vicinity of the solar system. Newton?s Shell Theorem would be applied to determine variations in apparent solar mass as the probe moves further out from the Sun. Application of this technique to the trajectories of Pioneer 10/11 reveals that the upper limit to WIMP concentration within ~60 AU of the Sun is ~0.2 Earth masses, as revealed in studies of the Pioneer Anomaly. If the published accuracy of the Pioneer acceleration measurements can be increased by an order of magnitude, probe trajectory measurements out to ~10,000 AU may confirm or falsify the hypothesis that WIMP mass within the solar vicinity is ~3X star mass. It is shown that a space-manufactured ~40-nm thick beryllium hollow-body solar sail deployed from a ~0.07 AU perihelion is a candidate spacecraft for such a mission. Possible science-team organization strategy for a ~100-year mission to ~10,000 AU is discussed. 相似文献
308.
Marc Jorba-Cuscó Ariadna Farrés Àngel Jorba 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(9):2812-2822
Solar sails change the natural dynamics of systems: Trajectories that are driven by gravitational forces can be displaced and changed because of the effect of Solar Radiation Pressure (SRP). Moreover, if the lightness number of the sail is large enough, the instability of certain orbits can be diminished and even removed. In this paper we modify two models for the motion of a probe in the Earth-Moon system that include the effect of Sun’s gravity to take also into account the effect of SRP. These models, the Bicircular Problem (BCP) and the Quasi-Bicircular Problem (QBCP), are periodic perturbations of the Earth-Moon Restricted Three Body Problem (RTBP). The models are modified to consider the effect of the SRP upon a solar sail. We provide examples of periodic orbits that are stabilized (or made less unstable) due to the effect of SRP. 相似文献
309.
霍尔推力器羽流对S波段电磁波信号有衰减作用,这对星上推力器与天线的布置策略有重要影响。为研究S波段电磁波的衰减程度,建立几何光路算法,对电磁波在等离子体羽流媒质中的传输衰减进行数值描述,并以试验所测的信噪比数据来验证算法精度。验证试验采用空间透射波法,在相同工况的试验与计算结果对比中,最大计算误差为26.1%,平均误差为7.3%;在趋势上,试验结果与计算结果保持一致。在此基础上,针对84个在轨典型工况进行S波段电磁波信噪比衰减计算,结果显示:羽流对电磁波的吸收作用是影响衰减的主要因素,衰减最大区域出现在天线位置0.3~0.6m、方向角15°~30°的区域,衰减值在-7~-4dB之间。该结果可为霍尔推力器与天线在卫星的布置提供参考依据。 相似文献
310.
The space-based Solar and Heliospheric Observatory (SOHO) is a joint venture of ESA and NASA within the frame of the Solar Terrestrial Science Programme (STSP), the first Cornerstone of ESA's long-term programme Space Science — Horizon 2000. The principal scientific objectives of the SOHO mission are: a) a better understanding of the structure and dynamics of the solar interior using techniques of helioseismology, and b) a better insight into the physical processes that form and heat the Sun's corona, maintain it and give rise to its acceleration into the solar wind. To achieve these goals, SOHO carries a payload consisting of 12 sets of complementary instruments which are briefly described here. 相似文献