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排序方式: 共有293条查询结果,搜索用时 78 毫秒
81.
82.
Spaceborne GPS receiver antenna phase center offset and variation estimation for the Shiyan 3 satellite 总被引:3,自引:2,他引:1
《中国航空学报》2016,(5):1335-1344
In determining the orbits of low Earth orbit (LEO) satellites using spaceborne GPS, the errors caused by receiver antenna phase center offset (PCO) and phase center variations (PCVs) are gradually becoming a major limiting factor for continued improvements to accuracy. Shiyan 3, a small satellite mission for space technology experimentation and climate exploration, was developed by China and launched on November 5, 2008. The dual-frequency GPS receiver payload delivers 1 Hz data and provides the basis for precise orbit determination within the range of a few centime-ters. The antenna PCO and PCV error characteristics and the principles influencing orbit determi-nation are analyzed. The feasibility of PCO and PCV estimation and compensation in different directions is demonstrated through simulation and in-flight tests. The values of receiver antenna PCO and PCVs for Gravity Recovery and Climate Experiment (GRACE) and Shiyan 3 satellites are estimated from one month of data. A large and stable antenna PCO error, reaching up to 10.34 cm in the z-direction, is found with the Shiyan 3 satellite. The PCVs on the Shiyan 3 satellite are estimated and reach up to 3.0 cm, which is slightly larger than that of GRACE satellites. Orbit validation clearly improved with independent k-band ranging (KBR) and satellite laser ranging (SLR) measurements. For GRACE satellites, the average root mean square (RMS) of KBR resid-uals improved from 1.01 cm to 0.88 cm. For the Shiyan 3 satellite, the average RMS of SLR resid-uals improved from 4.95 cm to 4.06 cm. 相似文献
83.
简要介绍了“风云二号”静止气象卫星的地面应用系统、主要包括指令控制与数据接收站、数据处理中心、卫星运行控制中心三大组成部分以及三者之间的信息流程,最后介绍了由该系统输出的气象产品。 相似文献
84.
L. Prange A. Jäggi R. Dach H. Bock G. Beutler L. Mervart 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
The gravity field model AIUB-CHAMP02S, which is based on six years of CHAMP GPS data, is presented here. The gravity field parameters were derived using a two step procedure: In a first step a kinematic trajectory of a low Earth orbiting (LEO) satellite is computed using the GPS data from the on-board receiver. In this step the orbits and clock corrections of the GPS satellites as well as the Earth rotation parameters (ERPs) are introduced as known. In the second step this kinematic orbit is represented by a gravitational force model and orbit parameters. 相似文献
85.
The African Regional Centre for Space Science and Technology Education in English (ARCSSTE-E) was inaugurated in November 1998, with a mandate for the development of indigenous skills, knowledge and capacity, through rigorous theory, research, applications, field exercises and pilot projects that can enhance socioeconomic development. The institution runs a nine-month Postgraduate Diploma (PGD) programme in the areas of Remote Sensing and Geographic Information Systems (RS/GIS); Satellite Communications; Satellite Meteorology and Global Climate; and Basic Space Science and Atmospheric Physics (BSS), as well as short courses and outreach programmes. This paper describes the impact of the space postgraduate diploma programmes in the African region, highlighting the capabilities of the centre. Using a survey of participants in its courses, it notes where changes are needed and makes recommendations to this end. 相似文献
86.
Model Development and Adaptive Imbalance Vibration Control of Magnetic Suspended System 总被引:1,自引:1,他引:1
Tang Liang Chen Yiqing 《中国航空学报》2007,20(5):434-442
对星载磁悬浮单框架控制力矩陀螺,建立其转子的平动与转动的动力学方程。所建模型反映了转子的动、静不平衡特性,以及转子运动与框架、星体运动的耦合关系。模型是主动磁悬浮控制与动框架效应分析的基础。对动、静不平衡量未知的转子,设计了自适应对中控制器。在分散PD、比例交叉反馈控制器与高低通滤波器的基础上,通过动、静不平衡量的辨识与补偿控制,使转子绕其惯量主轴旋转,衰减角动量交换执行机构高速转子因不平衡而对基座产生的干扰力,消除星上主要颤振源,达到降低卫星姿态抖动的目的。 相似文献
87.
88.
I. Büsching O.C. de Jager 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008
In this study, we investigate how restrictive the γ-ray emission from the Galactic center region, as seen by HESS and other Cherenkov air shower arrays, is against various models for cosmic ray injection. We derive diffusion coefficients which fit the observed spatial scales of diffuse γ-ray emission from the extended emission associated with the molecular clouds SgrA, B and C. Using these diffusion coefficients, we then obtain a limit for time scale of assumed recent proton acceleration near the SMBH, as the spatial size of SgrA∗ in VHE γ-rays has to be consistent with the observed unresolved HESS point source size at this position. The signal from this hadronic component may be mixed with the expected VHE inverse Compton emission from the nearby unresolved pulsar wind nebula. 相似文献
89.
A. Damiani E. Benedetti M. Storini C. Rafanelli 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(1):223-226
The International Heliophysical Year offers a good opportunity to develop and coordinate studies on the Sun–Earth system by using a large variety of simultaneous data obtained by satellite/spacecraft and ground based instruments. Among these data we recall the ones coming from solar and interplanetary medium observations, auroral, neutron monitor, geomagnetic field, ionospheric, meteorological, and other atmospheric observatories. In this context, an Information System for the Italian Research in Antarctica has started in 2003, aiming to collect information on the scientific research projects funded by the National Antarctic Research Program of Italy since its establishment (1985). It belongs to Joint Committee on Antarctic Data Management of Scientific Committee on Antarctic Research as Italian Antarctic Data Center. This project, as the Italian Polar Database, gathers also information on research activities conducted in North Pole regions. This Information System can be a relevant resource for capacity building associated with the International Heliophysical Year, especially for people involved in interdisciplinary researches. We describe the present status of the Italian Polar Data Center and its potential use. 相似文献
90.
叙述了CX1型无人机称重仪的组成与工作原理,推导了CX1型无人机总重量及重心的计算公式,对系统的测量误差进行了分析和修正。CX1型无人机机身细长,动力装置距离飞机重心较远,对飞行性能影响很大。CX1型无人机称重仪是检测CX1型无人机的专用地面检测设备,它可以自动检测称重台架上三个支撑点的重量,计算出CX1型无人机的总重量及重心,并将检测与计算结果在面板上显示出来,可以非常方便地实现CX1型无人机的重量和重心的调配。 相似文献