可展开式辐射器热控对航天器轨道调整的适应性分析

为提高航天器热控系统对轨道调整的适应能力，本文研究了与流体回路耦合的可展开式辐射器热控方案在不同轨道高度下的热控性能，分析了不同轨道高度时辐射器面临的热环境的影响，在不同轨道高度下比较了固定辐射器与可展开辐射器的热控特性。结果表明，随着辐射器展开角度的变化，辐射器吸收的空间热流随之发生变化，从而对热控系统的散热能力带来直接影响，调节辐射器的角度可以扩大其对外散热能力。在工程应用中，基于热控流体回路，通过调节可展开式辐射器的展开角度，可以有效提高航天器的轨道热适应能力。     

High velocity impact characterization of Al alloys for oblique impacts

This paper describes the experimental and computational analyses of a high velocity aluminum projectile impact on an Al6061-T6 spacecraft inner wall at different oblique angles. Al2017-T4 spherical projectiles of 5.56 mm in diameter and 0.25 g in weight were chosen within the velocity range of 1000±200 m/s due to the limitation of the light gas gun. The energy absorbed was calculated by measuring the velocities before and after impact on the inner wall. The energy absorbed by the wall and the remaining energy carried by the projectile helped to estimate the severity of further damage to inner components. Afterwards, validation was done by using the commercially available software LS-DYNA with a dedicated SPH. On average, a 10% energy absorption difference between experimentation and simulation was found. By using C-SCAN, the damage area proportion of the total inner wall to impact penetration hole area was found to be on average 6%, 26% and 53% greater than the projectile cross sectional area for the oblique angle impacts of 30°, 45°, and 60°, respectively. These findings helped to understand the relationship between the oblique impact event and the damage area on a spacecraft inner wall along with space debris cloud propagation and comparison with experimental results using LS-DYNA.     

GRB observed by IBIS/PICsIT in the MeV energy range

We present the preliminary results of a systematic search for GRB and other transients in the publicly available data for the IBIS/PICsIT (0.2–10 MeV) detector on board INTEGRAL. Lightcurves in 2–8 energy bands with time resolution from 1 to 62.5 ms have been collected and an analysis of spectral and temporal characteristics has been performed. This is the nucleus of a forthcoming first catalog of GRB observed by PICsIT.     

Analysis of total visual and CCD V-broadband observations of Comet C/1995 O1 (Hale-Bopp): 1995–2001

We developed a general method for determination of water production rates from groundbased visual observations and applied it to Comet Hale–Bopp. Our main objective is to extend the method to include total visual magnitude observations obtained with CCD detector and V filter in the analysis of total visual magnitudes. We compare the CCD V-broadband careful observations of Liller [Liller, W. Pre-perihelion CCD photometry of Comet 1995 O1 (Hale-Bopp). Planet. Space Sci. 45, 1505–1513, 1997; Liller, W. CCD photometry of Comet C/1995 O1 (Hale-Bopp): 1995–2000. Int. Comet Quart. 23(3), 93–97, 2001] with the total visual magnitude observations from experienced international observers found in the International Comet Quarterly (ICQ) archive. A data set of ∼400 CCD observations covering about the same 6 years time span of the ∼12,000 ICQ selected total visual magnitude observations were used in the analysis. A least-square method applied to the water production rates, yields power laws as a function of the heliocentric distances for the pre- and post-perihelion phases. The average dimension of the nucleus as well as its effective active area is determined and compared with values published in the literature.     

Occurrence rate of SAR arcs during the 23rd solar activity cycle

The occurrence rate of SAR arcs during 1997–2007 has been analyzed based on the photometric observations at the Yakutsk meridian (Maimaga station, corrected geomagnetic coordinates: 57°N, 200°E). SAR arcs appeared in 114 cases (∼500 h) during ∼370 nights of observations (∼3170 h). The occurrence frequency of SAR arcs increases to 27% during the growth phase of solar activity and has a clearly defined maximum at a decline of cycle 23. The SAR arc registration probability corresponds to the variations in geomagnetic activity in this solar cycle. The dates, intervals of UT, and geomagnetic latitudes of SAR arc observations at the Yakutsk meridian are presented.     

Discrete energy release in microwave emission in the preflare stage

Examples of solar microwave precursors and estimates of their energetic characteristics are discussed based on spectral investigations of the preflare activity.     

航天器弹性附件伸展动力学研究

利用动量矩定理推导出带伸展弹性板航天器的姿态动力学方程，在弹性板等速伸展的情况下，导出板的振动与伸展运动耦合微分方程，航天器姿态运动与板的伸展运动、振动耦合微分方程，通过龙格－库搭积分法得出了数值解，结果表明：弹性板等速伸展时，其振动的振幅随板长度的增长而增大，航天器姿态角速度随板长度的增长而减少。弹性板等速率越大，板振动的振幅越大。     

基于GPS/IMU/太阳敏感器的空间飞行器组合姿态确定

GPS定姿是GPS在空间飞行器上应用的一个重要方向 ,本文在建立GPS 惯性组件 太阳敏感器组合定姿系统的非线性模型的基础上 ,采用扩展卡尔曼滤波实现了该组合定姿方案。通过理论分析和仿真结果均验证了方案的可行性。为GPS定姿在空间飞行器的实际应用提供一定的参考。