共查询到20条相似文献,搜索用时 921 毫秒
1.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1986,6(4):187-190
A simple gamma ray telescope based on a time of flight triggering device has been constructed to measure medium energy photons (4–50 MeV). This instrument has been flown twice aboard stratospheric balloons. The results of these flights, used to separate the cosmic diffuse gamma-radiation from the atmospheric flux, using the growth curves, are presented. 相似文献
2.
3.
4.
R. Bu
ík K. Kudela A. V. Dmitriev S. N. Kuznetsov I. N. Myagkova S. P. Ryumin 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2002,30(12):2843-2848
According to the data from the SONG instrument on board the low altitude high inclination CORONAS-I satellite, the fluxes of gamma rays with energies between 120 keV and 8.3 MeV are reviewed. The observations were made during the interval from May 1994 to early July 1994. Comparison with energetic electron fluxes obtained from AE-8 model is done, and thus the gamma-ray production mechanism is discussed. Available data are used to investigate the fine spatial structure in the Brazilian anomaly, as well as to analyse outer zone of bremsstrahlung electrons. To do this, the L-B maps are constructed and energy spectral characteristics of gamma-ray fluxes are investigated. 相似文献
5.
基于SIMION软件的空间等离子体探测器的数值仿真 总被引:1,自引:0,他引:1
空间等离子体探测器采用带偏转板的柱形静电分析器作为传感器,具有大于320°探测视场,可探测约10eV~30keV的热等离子体。利用SIMION软件采用均匀随机抽样建立粒子源的方法仿真探测器的基本特性参数:静电分析器因子、能量分辨率、偏转板因子和偏转角。仿真结果与实测结果吻合很好。静电分析器因子的仿真与实测结果偏差为3.2%,能量分辨率仿真与实测结果偏差为1.5%,偏转角-偏转板因子的关系式与实测结果的相关系数为0.999 4。仿真结果可以有效地应用于该类仪器的设计和定标过程中。 相似文献
6.
Christopher B. Dreyer Kris Zacny John P.H. Steele James R. Schwendeman Gale Paulsen Robert C. Andersen John Skok 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
In this paper we present a conceptual design of a spaceborne instrument for the in situ production of rock thin sections on planetary surfaces. The in situ Automated Rock Thin Section Instrument (IS-ARTS) conceptual design demonstrates that the in situ production of thin sections on a planetary body is a plausible new instrument capability for future planetary exploration. Thin section analysis would reduce much ambiguity in the geological history of a sampled site that is present with instruments currently flown. The technical challenge of producing a thin section device compatible with the spacecraft environment is formidable and has been thought too technically difficult to be practical. Terrestrial thin section preparation requires a skilled petrographist, several preparation instruments that individually exceed typical spacecraft mass and power limits, and consumable materials that are not easily compatible with spaceflight. In two companion papers we present research and development work used to constrain the capabilities of IS-ARTS in the technical space compatible with the spacecraft environment. For the design configuration shown we conclude that a device can be constructed that is capable of 50 sample preparations over a 2 year lifespan with mass, power, and volume constraints compatible with current landed Mars mission configurations. The technical requirements of IS-ARTS (mass, power and number of samples produced) depend strongly on the sample mechanical properties, sample processing rate, the sample size and number of samples to be produced. 相似文献
7.
本文通过大量的实验数据,详细分析了失真仪的各种误差,指出了影响失真仪质量的原因,提出了合理判定仪器质量的方法和建议,为厂家提供了改进设计的思路。 相似文献
8.
9.
10.
从仪器的结构和性能特点方面,对虚拟仪器和传统仪器作了较详尽的比较,提出了“软件就是仪器”的新概念。为进一步阐明虚拟仪器的基本概念,列举并分析了VXI总线虚拟仪器的软件框架。 相似文献
11.
为了满足某无人机半实物仿真系统视景显示需要,针对视景界面复杂、显示数据种类多、实时性和流畅性要求高的特点,设计了基于GL Studio的组合虚拟仪表界面。详细介绍了组合虚拟仪表设计和实现过程,并通过VC++平台实现了网络通信和数据驱动仪表显示功能。仿真系统实际应用表明:该飞行组合仪表工作性能可靠,人机界面友好,具有良好的可重构性,满足不同无人机飞行仿真系统和飞行训练系统使用需求。 相似文献
12.
为了满足某无人机半实物仿真系统视景显示需要,针对视景界面复杂、显示数据种类多、实时性和流畅性要求高的特点,设计了基于GL Studio的组合虚拟仪表界面。详细介绍了组合虚拟仪表设计和实现过程,并通过VC++平台实现了网络通信和数据驱动仪表显示功能。仿真系统实际应用表明:该飞行组合仪表工作性能可靠,人机界面友好,具有良好的可重构性,满足不同无人机飞行仿真系统和飞行训练系统使用需求。 相似文献
13.
14.
J.R. Drummond D. Turner A. Ashton 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1985,5(1):73-76
The determination of the line-of-sight with reference to the atmospheric horizontal is critical to the correct interpretation of signals from an emission-sensing, limb-scanning instrument. The use of signals from a two-sided, limb-scanning instrument, the University of Toronto Balloon Radiometer, to determine the beam position relative to the atmospheric horizontal is discussed. Some preliminary results from the engineering flight of the instrument are presented. 相似文献
15.
虚拟量仪——一种新的量仪设计思想 总被引:1,自引:0,他引:1
从虚拟仪器和虚拟现实技术出发,提出了虚拟量仪这一新概念,并对虚拟量仪的定义、特点、优点、结构形式以及虚拟量仪设计的基本思想、基本内容和关键技术作了分析。 相似文献
16.
纤维/树脂浸润测试仪的研制与应用 总被引:1,自引:0,他引:1
针对复合材料成型工艺的特点,依据毛细原理,研制了浸润性能测试仪.该测试仪包括浸润质量测试系统与温度控制系统,能够定量测试在较宽的温度范围内发生浸润的速率和浸润程度.对该测试仪的准确性与稳定性进行了校准与标定,并运用该仪器研究了纤维种类、树脂粘度和纤维体积含量对树脂/纤维浸润性能的影响规律.研究结果表明该设备为研究各类复合材料中增强材料与基体间的浸润性能提供了方便的测试手段,对指导复合材料制备工艺具有较高的参考价值. 相似文献
17.
提出采用匹配函数描述测试点与仪器端口的匹配程度,用来指导自动测试系统仪器选型和资源配置.匹配函数采用面向信号的方法构建,综合了测点信号属性与仪器性能参数、仪器可靠性、仪器成本、仪器操作复杂度等因素,使得仪器选型和资源配置策略的制定更符合工程需要.给出了资源配置策略和算法,并对资源配置进行了并行测试优化.通过给出一个典型实例,证明该方法能有效降低测试成本,增强系统可靠性,提高测试效率和吞吐量,并为自动测试系统硬件设计的自动化奠定了基础. 相似文献
18.
19.
20.
Sebastian E. Schroeder Andreas Kullmann Peter Preusse Fred Stroh Katja Weigel Manfred Ern Peter Knieling Friedhelm Olschewski Reinhold Spang Martin Riese 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009,43(12):1910-1917
The CRISTA-NF instrument is the airborne version of the CRISTA satellite infrared limb sounder. It has been successfully flown on the Geophysica research airplane during a test campaign in July 2005, during the SCOUT-O3 Tropical Aircraft Campaign in November/December 2005 and during the AMMA campaign in August 2006. Radiance calibrations of the airborne instrument are more complex compared to the satellite instrument because the vacuum shell of CRISTA-NF is confined by a ZnSe (zinc–selenide) window and the detectors can thermally drift during measurement flights. By comprehensive radiance calibrations with a blackbody source the window’s emissivity and transmissivity are determined and the dependence of the instrument sensitivity on the detector temperature is characterized. Taking these effects into account, the remaining radiance error of the calibration is smaller than 3%. 相似文献