首页 | 本学科首页   官方微博 | 高级检索  
相似文献
 共查询到20条相似文献,搜索用时 203 毫秒
1.
本文指出了太阳射电快速记录系统中方波隔离放大器研制的必要性,并简要介绍了设计出发点,工作原理,设计和主主要技术指标的测试。  相似文献   

2.
LEO卫星轨道设计中的主要摄动源影响评估   总被引:3,自引:0,他引:3  
对地球低轨道卫星(LEO)轨道设计中的摄动力模型进行了分析,并估计了其量级。然后针对用于GPS无线电掩星的LEO卫星轨道设计对掩星地面测点稳定性的要求,对力学模型进行了取舍,同时估计了各摄动力模型对轨道设计目标的影响。  相似文献   

3.
有限元分析技术在空间太阳望远镜结构设计中的应用   总被引:2,自引:0,他引:2  
有限元分析技术是现代工程领域中进行结构分析的一种数值方法,已经广泛应用于天文仪器设计。它可使设计者了解被设计对象相应的特性,发现强度或刚度等方面的薄弱点,从而改进和优化设计。以空间太阳望远镜主桁架和主镜室的设计为例,从几何建模、单元划分入手,对静力学分析、模态分析、动态响应和热分析等各方面在空间太阳望远镜设计中的应用进行了阐述;分析了有限元分析存在的误差、产生的原因以及如何减少误差;叙述了有限元分析技术应用于天文仪器尤其是空间天文仪器的发展趋势。  相似文献   

4.
本文介绍棱镜分光光度仪PSPO的光学设计结果.PSPO以TH7832双线CCD作为系统探测器,可同时观测0.365-1.0微米波长范围内的天体及周围背景的低色散光谱.仪器的入射焦比为F/18,平均光谱分辨率约为10nm.本文简单介绍了PSPO的光学调整,并给出了波长校正实验和配备名古屋大学50公分望远镜进行试观测的结果.设计和实验结果表明,光学设计很好地满足了天文课题对仪器的设计要求,PSPO已可以应用于天文观测.  相似文献   

5.
胡小工  黄珹 《天文学进展》2001,19(2):289-294
讨论满足约束条件的月球卫星飞行轨道的设计问题,将约束条件分类为只与太阳,月球,地球,飞行器和观测站之间的相对位置有关的运行学约束条件以及涉及到飞行器轨道运行的动力学约束条件,在考虑月球卫星轨道的受力情况后,给出一种准确快速地计算和设计满足约束条件的标准飞行轨道的方法,并应用于不同约束条件下月球卫星的轨道预设计,初步讨论了轨道设计的误差分析,轨道跟踪及实时精密定轨等正在进行的其它相关工作。  相似文献   

6.
分光仪PSP0的光学设计   总被引:1,自引:0,他引:1  
姚永强  张振超 《天文学报》1997,38(1):105-112
本文介绍棱镜分光光度仪PSP0的光学设计结果。PSP0以TH7832双线CCD作为系统探测器,可同时观测0.365-1.0微米波长范围内的天体及周转背景的低色散光谱。仪器的入射焦比为F/18,平均光谱分辨率约为10nm。本文简单介绍了PSP0的光学调整,并给出了波长校正实验和配备名古屋大学50公分望远镜进行试观测的结果。设计和实验结果表明,光学设计很好地满足了天文课题对仪器的设计要求,PSP0已可  相似文献   

7.
本文指出了子午环光栏自动控制系统研制的必要性,并简要介绍了控制原理,结果表明,该控制部分设计合理大大简便了操作。  相似文献   

8.
光电测微器是中-丹水平子午环最关键的部分.本文介绍了数据采集系统的设计思想.根据长期对仪器的测试和观测结果分析,表明系统完全达到设计要求,同时为下一步改装成CCD终端,观测极限星等达17m.5提供了可行的方案.  相似文献   

9.
简单介绍了混频电路频率变换的概念、常用的几种简单的混频电路和设计混频电路要考虑的几个性能参数,详细阐述了GPS接收机射频前端电路中的下变频设计。  相似文献   

10.
介绍了云南天文台1.2m望远镜激光光学净化室自动控制恒温系统的建立,实现了自动风流循环、净化空气,自动控制加热器使净化室内温度保持在恒定范围,从而保证光学系统工作在最佳状态。整个自动控制系统的新设计是建立在只具有风机、加热器两套人工控制装置的原设计基础上进行的。  相似文献   

11.
The reference system defined by Veis and currently used for computing satellite orbits is not sufficiently accurate for some scientific applications, considering the new accuracy of laser data. We have therefore defined another orbital reference system with associated apparent forces. The reference system chosen is the mean celestial system 1970.0. The motion of a satellite is numerically integrated in the instantaneous celestial system (sideral system), taking into account all the complementary forces due to precession and nutation. The complete set of formulas is given here and has been introduced in a differential orbital improvement program.  相似文献   

12.
一个巨型望远镜方案   总被引:4,自引:0,他引:4  
提出一个有特色的巨型望远镜(FGT)方案.其主镜口径为30米,主焦比为1.2,由1095块圆环形子镜构成.采用地平式装置.光学系统包括Nasmyth系统、折轴(Coude)系统和一个大视场系统.提出一个由4个镜面组成的新的Nasmyth系统,在约10′的视场范围内像斑小于爱里斑,达到衍射极限.比传统的Nasmyth系统的衍射极限视场大得多.可在这样的大视场内同时作好几个小区域的衍射极限的观测.当由Nasmyth系统转换到折轴系统和大视场系统时,采用主动光学技术改变子镜的面形、倾斜和平移,产生一个新的主镜面形,使折轴系统和大视场系统都能得到很好的像质.大视场系统的视场直径25′,场曲轻微,并有可能校正大气色散.给出了子镜面形和位置的公差,并讨论了望远镜的装置和结构,方案中的特色和创新对未来大望远镜的研制有普遍意义.  相似文献   

13.
A configuration for the Future Giant Telescope is proposed. It is a 30m telescope with segmented primary mirror and alt-azimuth mounting. The aspherical f/1.2 primary mirror is made up of 1095 partial annular submirrors. The optical system includes a Nasmyth system, a coude system and a wide field system. The Nasmyth system has a novel design with four mirrors and provides a ∼10 arcmin field of diffraction-limited images, a much larger field than can be obtained by the traditional Nasmyth system. Several diffraction-limited observations each over a small field, can be carried out simultaneously. By applying active optics to change the shape, tip, tilt and piston of the submirrors, thereby to effect a new aspherical surface of the primary, excellent quality images can be obtained for the coude system and the wide field system. The wide field system has a field of 25 arcmin, the focal surface is only slightly curved and the atmospheric dispersion could be corrected. The tolerances of the surface shape and position for the submirrors, and the telescope mounting and structure are also discussed. The innovations in this configuration should have a general significance for future giant telescopes.  相似文献   

14.
Linear dispersion relations are solved numerically for collisionless self-gravitating systems. The results are compared to those of hydrodynamic approach. Both theories yield similar dispersion relations, with predictions of instability when the system is cold enough. In a collisionless system, however, the perturbation is found to die away without oscillations when the system is stable. A mixed system of hot-component particles and cold-component particles is also studied. The stability of such system is dominated by the temperature of the cold particles. Again, the oscillatory behaviour is not found in this case, regardless of the stability of the system.  相似文献   

15.
基于MYSQL/LINUX 的LAMOST数据库设计与实现   总被引:1,自引:0,他引:1  
大天区面积多目标光纤光谱天文望远镜(LAMOST)将被建成,在投入使用之前设计开发出全自动处理光谱的软件系统是必需的。完善的数据库系统是该光谱处理软件不可缺少的一部分。本文分析了LAMOST对数据库的需求,设计并实现了基于MYSQL/LINUX的LAMOST数据库系统并对该系统进行了初步测试。  相似文献   

16.
太阳磁像仪是开展太阳磁场观测研究的核心仪器,其中的稳像系统是空间太阳磁像仪的关键技术之一,针对深空探测卫星系统对载荷重量、尺寸限制严苛的要求,设计了基于图像自校正方法的稳像观测系统.介绍了一套基于现场可编程门阵列(Field-Programmable Gate Array, FPGA)和数字信号处理器(Digital Signal Processor, DSP),通过基于自相关算法的高精度稳像方法设计,并结合精确偏振调制、准确交替采样控制等系统软硬件设计,克服由于卫星平台抖动、指向误差等因素造成的图像模糊,实现实时相关、校正、深积分的稳像观测系统.针对像素尺寸为1 K×1 K、帧频为20 fps的CMOS (Complementary Metal Oxide Semiconductor)探测器,实现了1像元以内的实时稳像观测精度.在完成实验室测试后, 2021年6月18日在国家天文台怀柔太阳观测基地35 cm太阳磁场望远镜上开展了实测验证,结果表明该系统能够有效地完成太阳磁像仪自校正稳像观测,获得了更高分辨率的太阳磁场数据.稳像系统的成功研制不仅可以为深空太阳磁像仪的研制提供轻量化、高...  相似文献   

17.
守时设备故障的自动诊断和报警系统设计   总被引:1,自引:0,他引:1  
为了及时发现守时主系统运行中出现故障概率最高的设备,降低比对数据的出错率,提高守时精度及比对数据的可靠性和完整性,设计了一种守时设备故障的自动诊断和报警系统。该系统采用专家系统故障诊断方法,通过对守时比对系统的时间比对数据的实时监测和分析,发现比对数据异常,及时启动故障自动诊断系统,通过报警系统报告发生故障的可能设备,实现故障的及时发现和尽快排除。结果表明,该守时设备故障的自动诊断和报警系统达到了预期目标。  相似文献   

18.
A reference system is a relation connecting observables and their mathematical represententions. The principle of general relativity assures that any sort of coordinate system can be used to describe physical phenomena. Thus, any reference system is only a convention, There is no absolutely true reference system. Instead, people seek for a best reference system, whose meaning may differ thus need to clarify, Taking an example from Earth rotation, we discuss how to find such a best reference system. The definition of the best system will change as scientific understandings deepen and computational environments develop. Therefore, we can not stop improving reference systems. However, when replacing an existing widely-spread system, one must take great care to minimize the inconvenience caused by its transition, especially the inconvenience which users might endure. The Standards Of Fundamental Astronomy (SOFA) project being conducted by the IAU WG on Astronomical Standards has the opportunity to ease this troublesome task. The World Wide Web (WWW) will be a main device to realize the project, namely to provide working standards including reference systems to the world.  相似文献   

19.
The ALFA laser subsystem uses a 4 watt continuous wave laser beam to produce an artificial guide star in the mesospheric sodium layer as a reference for wavefront sensing. In this article we describe the system design, focusing on the layout of the beam relay system. It consists of seven mirrors, four of which are motor-controlled in closed loop operation accounting for turbulences inside the dome and flexure of the main telescope.The control system features several computers which are located close to analysis and control units. The distribution of the tasks and their interaction is presented, as well as the graphical user interface used to operate the complete system. This is followed by a discussion of the aircraft detection system ALIENS. This system shuts off the laser beam when an object passes close to the outgoing laser.  相似文献   

20.
The system gain of two CCD systems in regular use at the Vainu Bappu Observatory, Kavalur, is determined at a few gain settings. The procedure used for the determination of system gain and base-level noise is described in detail. The Photometrics CCD system at the 1-m reflector uses a Thomson-CSF TH 7882 CDA chip coated for increased ultraviolet sensitivity. The gain is programme-selected through the parameter ‘cgain’ varying between 0 and 4095 in steps of 1. The inverse system gain for this system varies almost linearly from 27.7 electrons DN-1 at cgain = 0 to 1.5 electrons DN-1 at cgain = 500. The readout noise is ≲ 11 electrons at cgain = 66. The Astromed CCD system at 2.3-m Vainu Bappu Telescope uses a GEC P8603 chip which is also coated for enhanced ultraviolet sensitivity. The amplifier gain is selected in discrete steps using switches in the controller. The inverse system gain is 4.15 electrons DN-1 at the gain setting of 9.2, and the readout noise ∼ 8 electrons.  相似文献   

设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号