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961.
962.
针对卫星测控天线日照温度场产生的热变形影响天线电性能问题,提出了一种预测天线极端温度工况的方法.该方法将太阳照射参数与天线面板方程有效结合起来,求得天线面板的太阳直射点运动轨迹,从而确定天线姿态参数.在Ⅰ-DEAS中建立该姿态的模型,同时引入环境因素的影响,进行瞬态仿真分析,预测天线的极端温度工况.通过试验天线,验证理论计算太阳直射点运动轨迹与极端温度预测方法的正确性. 相似文献
963.
Zhongchao Liang Haibo Gao Liang DingZongquan Deng Jianjun Qu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
To investigate and improve the mobility of the Lunar Roving Vehicle (LRV), it is necessary to consider the mechanical properties of the interaction between the wheels and the ground. In this paper, a new solution method, the forced-slip solution method, which uses a semi-empirical approach, was presented. That is, given the wheel’s vertical load and drawbar pull or driving torque as known input values, the unknown slip ratio can be resolved. The alternative method involves predicting the mechanics for a given slip ratio. The proposed method correlates better with actual wheel movements, and by studying a single wheel, this solution method can also be used to resolve the mechanical properties of the front and rear wheels in a four-wheel-drive (4WD) LRV configuration. It can also be used to consider the multi-pass effect of the rear wheels on lunar soil. The calculation results show that the 4WD LRV driving efficiency varies with the position of the center of mass. Thus, the LRV driving efficiency can be optimized by adjusting the position of its center of mass. 相似文献
964.
L. Perna M. Pezzopane E. Zuccheretti P.R. Fagundes R. de Jesus M.A. Cabrera R.G. Ezquer 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
This paper is focused on unusual nighttime impulsive electron density enhancements that are rarely observed at low latitudes on a wide region of South America, under quiet and medium/high geomagnetic conditions. The phenomenon under investigation is very peculiar because besides being of brief duration, it is characterized by a pronounced compression of the ionosphere. The phenomenon was studied and analyzed using both the F2 layer critical frequency (foF2) and the virtual height of the base of the F region (h′F) values recorded at five ionospheric stations widely distributed in space, namely: Jicamarca (−12.0°, −76.8°, magnetic latitude −2.0°), Peru; Sao Luis (−2.6°, −44.2°, magnetic latitude +6.2°), Cachoeira Paulista (−22.4°, −44.6°, magnetic latitude −13.4°), and São José dos Campos (−23.2°, −45.9°, magnetic latitude −14.1°), Brazil; Tucumán (−26.9°, −65.4°, magnetic latitude −16.8°), Argentina. In a more restricted region over Tucumán, the phenomenon was also investigated by the total electron content (TEC) maps computed by using measurements from 12 GPS receivers. A detailed analysis of isoheight ionosonde plots suggests that traveling ionospheric disturbances (TIDs) caused by gravity wave (GW) propagation could play a significant role in causing the phenomenon both for quiet and for medium/high geomagnetic activity; in the latter case however a recharging of the fountain effect, due to electric fields penetrating from the magnetosphere, joins the TID propagation and plays an as much significant role in causing impulsive electron density enhancements. 相似文献
965.
针对X射线脉冲星导航中,传统的扩展卡尔曼滤波(EKF)算法因为线性化需要从而忽略观测模型高阶项导致较大截断误差的问题,提出一种适用于脉冲星导航的改进线性观测方程。首先,详细分析了观测方程简化过程中会造成截断误差的周年视差效应及引力延迟效应的物理意义,介绍了2个高阶项的数学模型,并对2项进行了详细的数值分析。其次,利用泰勒展开等方式,将2个高阶项进行线性化处理,建立一种改进的线性观测方程。最后,利用地球卫星轨道数据,将2个线性观测方程分别应用到脉冲星导航的EKF解算中验证改进线性观测方程的有效性。结果表明,在考虑高阶项影响的条件下,改进的线性观测方程均能保证250 m和2 m/s以内的位置和速度估计误差而且对高阶项变化表现出一定的鲁棒性,但传统的简化线性观测方程却会导致发散。 相似文献
966.
雷达导引头跟踪低空飞行目标时,其仰角跟踪误差会受多径传播的严重干扰.一般的"小平面"方法计算漫反射时,采用均匀分割地形的方法,这种分割法在大擦地角,目标距离地面较低的情况下,误差较大,并且计算时间较长.提出了非均匀分割的改进的"小平面"法,分析了4条回波路径的影响.采用了闭环跟踪法计算仰角误差,并利用改进的"小平面"法计算电磁波在起伏地/海面上的漫反射,可以较为真实的模拟导引头在跟踪低空目标时的仰角跟踪误差,并可以大大缩短计算时间. 相似文献
967.
传统的光学谐振陀螺(ROG)把背向散射作为重要误差源之一,须尽量抑制其影响.在光学谐振腔的品质因数极高时,背散光得到足够的增强,不能再被简单地视为噪声.背向散射会引发模式劈裂,所形成的劈裂模谐振频率会随腔体旋转角速率发生变化.结合Sagnac效应,修正有源光学谐振腔模式劈裂传感原理的数学模型,推导出腔体旋转角速率与劈裂值的映射关系式.通过仿真分析不同掺杂增益系数以及不同光纤锥耦合强度下的反射谱线,发现谐振腔工作在欠耦合区域更适合角速率测量.掺杂增益介质可以提高品质因数,减小谐振峰线宽,使得模式劈裂谱线更容易观测.理论与计算机仿真分析表明品质因数为108的光学微腔测量分辨率可达10-6(°)/s,所提出的角速率敏感机制很有应用前景. 相似文献
968.
969.
Burong Hu Jiayun Zhu Hongning Zhou Tom K. Hei 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
A major concern for bystander effects is the probability that normal healthy cells adjacent to the irradiated cells become genomically unstable and undergo further carcinogenesis after therapeutic irradiation or space mission where astronauts are exposed to low dose of heavy ions. Genomic instability is a hallmark of cancer cells. In the present study, two irradiation protocols were performed in order to ensure pure populations of bystander cells and the genomic instability in their progeny were investigated. After irradiation, chromosomal aberrations of cells were analyzed at designated time points using G2 phase premature chromosome condensation (G2-PCC) coupled with Giemsa staining and with multiplex fluorescent in situ hybridization (mFISH). Our Giemsa staining assay demonstrated that elevated yields of chromatid breaks were induced in the progeny of pure bystander primary fibroblasts up to 20 days after irradiation. mFISH assay showed no significant level of inheritable interchromosomal aberrations were induced in the progeny of the bystander cell groups, while the fractions of gross aberrations (chromatid breaks or chromosomal breaks) significantly increased in some bystander cell groups. These results suggest that genomic instability occurred in the progeny of the irradiation associated bystander normal fibroblasts exclude the inheritable interchromosomal aberration. 相似文献
970.