描述 sentinelhub Python软件包允许用户发出OGC（WMS和WCS）Web请求，以在您的Python脚本中下载和处理卫星图像。 它支持Sentinel-2 L1C和L2A，Sentinel-1，Landsat 8，MODIS和DEM数据源。 该软件包还支持从Amazon Web Service获取数据。 它可以使用Sentinel-2 L1C图像提供来自公共存储桶的数据，也可以使用Sentinel-2 L2A图像提供请求者支付的存储桶。 如果指定了下载的数据，则可以ESA .SAFE格式存储（支持所有类型的.SAFE格式）。 安装 该软件包需要Python版本> = 3.6并已安装C / C ++编译器。 该软件包在PyPI软件包管理器上可用，并且可以与 $ pip install sentinelhub --upgrade 或者，可以从conda-forge渠道将软件包与Conda一起安装 conda install -c conda-forge sentinelhub 要手动安装软件包，请克隆存储库并 $ python setup.py build $ pytho

satellite tool kit是由美国Analytical Graphics公司开发的一款在航天领域处于领先地位的商业分析软件。STK支持航天任务的全过程，括设计、测试、发射、运行和任务应用。 STK提供分析引擎用于计算数据、并可显示多种形式的二维地图，显示卫星和其它对象如运载火箭、导弹、飞机、地面车辆、目标等。STK的核心能力是产生位置和姿态数据、获取时间、遥感器覆盖分析。STK专业版扩展了STK的基本分析能力，包括附加的轨道预报算法、姿态定义、坐标类型和坐标系统、遥感器类型、高级的约束条件定义，以及卫星、城市、地面站和恒星数据库。对于特定的分析任务，STK提供了附加分析模块，可以解决通信分析、雷达分析、覆盖分析、轨道机动、精确定轨、实时操作等问题。另外，STK还有三维可视化模块，为STK和其它附加模块提供领先的三维显示环境。

卫星轨道动力学模型方法及应用，包含基础动力学建模等相关内容。内容为英文版。

通过各种气象数据生成卫星云图,雷达,雨量,风力风向,温度图

satellite tool kit是由美国Analytical Graphics公司开发的一款在航天领域处于领先地位的商业分析软件。STK支持航天任务的全过程，括设计、测试、发射、运行和任务应用。 STK提供分析引擎用于计算数据、并可显示多种形式的二维地图，显示卫星和其它对象如运载火箭、导弹、飞机、地面车辆、目标等。STK的核心能力是产生位置和姿态数据、获取时间、遥感器覆盖分析。STK专业版扩展

《卫星通信系统工程》（Satellite Communications Systems Engineering：Atmospheric Effects, Satellite Link Design and System Performance）英文原版，Louis J. Ippolito, Jr.著。本书在对卫星通信系统组成、卫星本体、卫星运行轨道介绍的基础上，提供了一套系统的卫星通信链路设计和组网运行设计的方法。重点讲述了卫星通信链路计算与评估方法，大气对卫星通信的影响模型、预测方法、经验取值、减轻大气对无线电信号衰减的途径，卫星多址传输方法及移动卫星通信信道设计中的特殊因素等。

The new version of 6S (4.1) is available: download: 6sv4.1.tar.Z from kratmos.gsfc.nasa.gov (128.183.253.183) (use ftp for transfer, user:anonymous passwd:"your email") then change directory to 6S NB:6sv4.1.tar.Z is compressed (standart unix compress) Please register to the user mailing list by writing to: 6s@kratmos.gsfc.nasa.gov The MICROSOFT WORD document (version 6.0 for Macintosh, in AppleSingle format) of the manual is also available. It has been split in 3 parts : 6smanv2.0_P1_msw 6smanv2.0_P2_msw 6smanv2.0_P3_msw Make sure you download the files in binary mode (either by ftp or Fetch). A compressed version of the files is also available : 6smanv2.0_P1_msw.Z 6smanv2.0_P2_msw.Z 6smanv2.0_P3_msw.Z Use the "uncompress" unix command to retrieve the original Word documents, prior to transfer them to Mac or PC. A PostScript and a PDF version of the manual are also available : 6smanv2.0_P1.ps, 6smanv2.0_P2.ps, 6smanv2.0_P3.ps 6smanv2.0_P1.pdf, 6smanv2.0_P2.pdf, 6smanv2.0_P3.pdf

Mohinder S. Grewal的第三版Global Navigation Satellite Systems, Inertial Navigation, and Integration [ISBN: 978-1118447000]。 An updated guide to GNSS, and INS, and solutions to real-world GNSS/INS problems with Kalman filtering Written by recognized authorities in the field, this third edition of a landmark work provides engineers, computer scientists, and others with a working familiarity of the theory and contemporary applications of Global Navigation Satellite Systems (GNSS), Inertial Navigational Systems, and Kalman filters. Throughout, the focus is on solving real-world problems, with an emphasis on the effective use of state-of-the-art integration techniques for those systems, especially the application of Kalman filtering. To that end, the authors explore the various subtleties, common failures, and inherent limitations of the theory as it applies to real-world situations, and provide numerous detailed application examples and practice problems, including GNSS-aided INS (tightly and loosely coupled), modeling of gyros and accelerometers, and SBAS and GBAS. Drawing upon their many years of experience with GNSS, INS, and the Kalman filter, the authors present numerous design and implementation techniques not found in other professional references. The Third Edition includes: Updates on the upgrades in existing GNSS and other systems currently under development Expanded coverage of basic principles of antenna design and practical antenna design solutions Expanded coverage of basic principles of receiver design and an update of the foundations for code and carrier acquisition and tracking within a GNSS receiver Expanded coverage of inertial navigation, its history, its technology, and the mathematical models and methods used in its implementation Derivations of dynamic models for the propagation of inertial navigation errors, including the effects of drifting sensor compensation parameters Greatly expanded coverage of GNSS/INS integration, including derivation of a u

使用两行元素(TLE)文件，计算指定卫星的实时位置和姿态

哈夫曼经典之作，学习gps很好的参考书； Global Positioning System (GPS), originally Navstar GPS,[1][2] is a space-based radionavigation system owned by the United States government and operated by the United States Air Force. It is a global navigation satellite system that provides geolocation and time information to a GPS receiver anywhere on or near the Earth where there is an unobstructed line of sight to four or more GPS satellites.[3]