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针对J2摄动和大气摄动导致低轨编队卫星构型破坏的情况,基于高斯摄动方程给出了以平均轨道根数为被控制量的脉冲控制模型。利用法向脉冲调整轨道倾角和升交点赤经偏差,在轨道上2个位置施加径向和切向脉冲调整其余轨道根数偏差从而修正卫星编队构形。最后通过数值仿真验证了算法的简单性、有效性。 相似文献
224.
R. Sridharan Tirtha Pratim Das S.M. Ahmed Gogulapati Supriya Anil Bhardwaj J.A. Kamalakar 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
In the past, clues on the potential radiogenic activity of the lunar interior have been obtained from the isotopic composition of noble gases like Argon. Excess Argon (40) relative to Argon (36), as compared to the solar wind composition, is generally ascribed to the radiogenic activity of the lunar interior. Almost all the previous estimates were based on, ‘on-the-spot’ measurements from the landing sites. Relative concentration of the isotopes of 40Ar and 36Ar along a meridian by the Chandra’s Altitudinal Composition Explorer (CHACE) experiment, on the Moon Impact Probe (MIP) of India’s first mission to Moon, has independently yielded clues on the possible spatial heterogeneity in the radiogenic activity of the lunar interior in addition to providing indicative ‘antiquity’ of the lunar surface along the ground track over the near side of the moon. These results are shown to broadly corroborate the independent topography measurements by the Lunar Laser Ranging Instrument (LLRI) in the main orbiter Chandrayaan-1. The unique combination of these experiments provided high spatial resolution data while indicating the possible close linkages between the lunar interior and the lunar ambience. 相似文献
225.
B.O. Adebesin J.O. Adeniyi I.A. Adimula B.W. Reinisch 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
The nighttime vertical E × B drifts velocities of the F2-region were inferred from the hourly hmF2 values obtained from ionosonde data over an African equatorial station, Ilorin (8.50oN, 4.68oE; dip lat. 2.95o) during period of low solar activity. For each season, the plasma drift Vz is characterized by an evening upward enhancement, then by a downward reversal at 1900 LT till around 0000 LT, except for June solstice. This was explained using the Rayleigh–Taylor (R-T) instability mechanism. The occasional drift differences in Vz obtained by inferred and direct measurement over Ilorin and Jicamarca, respectively are reflective of the importance of chemistry and divergent transport system due to both the E region electric and magnetic fields instead of simple motions. The pre-reversal enhancement (PRE) magnitude is higher during the equinoctial months than the solsticial months over Jicamarca, highest during December solstice and the equinoctial months over Ilorin, suggesting the dominance of higher E × B fountain during equinoxes at both stations. The lowest PRE magnitude was in June solstice. The appearance of post-noon peak in NmF2 around 1700 LT is highest during the equinoctial months and lowest during the solsticial period. A general sharp drop in NmF2 around 1800 LT is distinct immediately after sunset, lowest during June solstice and highest in March equinox. Our result suggests that between 0930 and 2100 LT, the general theory that vertical drifts obtained by digisonde measurements only match the E × B drift if the F layer is higher than 300 km is reliable, but does not hold for the nighttime period of 2200–0600 LT under condition of solar minima. Hence, the condition may not be sufficient for the representation of vertical plasma drift at nighttime during solar minima. This assertion may still be tentative, as more equatorial stations needed to be studied for better confirmation. 相似文献
226.
M. Ogurtsov M. Lindholm R. Jalkanen S.V. Veretenenko 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
A new summer temperature proxy was built for northern Fennoscandia in AD 1000–2004 using parameters of tree growth from a large region, extending from the Swedish Scandes to the Kola Peninsula. It was found that century-scale (55–140 year) cyclicity is present in this series during the entire time interval. This periodicity is highly significant and has a bi-modal structure, i.e. it consists of two oscillation modes, 55–100 year and 100–140 year variations. A comparison of the century-long variation in the northern Fennoscandian temperature proxy with the corresponding variations in Wolf numbers and concentration of cosmogenic 10Be in glacial ice shows that a probable cause of this periodicity is the modulation of regional climate by the secular solar cycle of Gleissberg. This is in line with the results obtained previously for a more limited part of the region (Finnish Lapland: 68–70° N, 20–30° E). Thus the reality of a link between long-term changes in solar activity and climate in Fennoscandia has been confirmed. Possible mechanisms of solar influence on the lower troposphere are discussed. 相似文献
227.
由于高能电子辐射的长期照射,新一代太阳X射线探测器硅漂移传感器的探测性能可能发生变化.通过用电子放射源模拟空间电子对硅漂移探测器进行辐射照射试验,以测试电子照射对传感器能量分辨率、效率、信号幅度等性能的影响.试验结果表明,长期的电子照射造成硅漂移探测器面损伤和体损伤,使其漏电流增大,信号幅度减小,能量分辨率也受到照射的影响,而探测效率未发生变化. 相似文献
228.
针对无人机低空小捷径飞行要求,分析了无人机飞行航路偏差,计算了飞行安全可靠度,对无人机安控策略进行了设计,确保了小捷径航路飞行要求。 相似文献
229.
地球静止轨道卫星硅太阳电池在轨特性分析 总被引:1,自引:1,他引:0
空间辐照效应的影响,使太阳电池输出功率随其在轨时间的推移而逐渐衰减。文章以2颗在轨的地球静止轨道卫星为研究对象,对某类我国自主研发的硅太阳电池的在轨输出功率衰减率进行了分析。并针对所获得的相关遥测参数,通过数值统计与数学分析的方法,采用确定的计算公式得出太阳电池阵的总输出电流,用以表征其输出功率。文章提出了一种曲线平移... 相似文献
230.
Vaios Lappas Nasir Adeli Lourens Visagie Juan Fernandez Theodoros Theodorou Willem Steyn Matthew Perren 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
CubeSail is a nano-solar sail mission based on the 3U CubeSat standard, which is currently being designed and built at the Surrey Space Centre, University of Surrey. CubeSail will have a total mass of around 3 kg and will deploy a 5 × 5 m sail in low Earth orbit. The primary aim of the mission is to demonstrate the concept of solar sailing and end-of-life de-orbiting using the sail membrane as a drag-sail. The spacecraft will have a compact 3-axis stabilised attitude control system, which uses three magnetic torquers aligned with the spacecraft principle axis as well as a novel two-dimensional translation stage separating the spacecraft bus from the sail. CubeSail’s deployment mechanism consists of four novel booms and four-quadrant sail membranes. The proposed booms are made from tape-spring blades and will deploy the sail membrane from a 2U CubeSat standard structure. This paper presents a systems level overview of the CubeSat mission, focusing on the mission orbit and de-orbiting, in addition to the deployment, attitude control and the satellite bus. 相似文献