Graphical solution for space applications

R.B. Inampudi
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Abstract

Graphical solution for space applications is aimed at determining for spacecraft operation planning. The software basically gives the ground-trace and visibility pattern over the selected ground station. Ground-trace of a spacecraft is a path trace by the pierce point of a ray dropped from a given spacecraft in such a direction that it intersects normally the surface of the planet about which motion occurs. In the generation of the ground-trace the user is requested to give the starting time and closing time of the satellite to generate ground-trace. To generate the latitude and longitude values of the visibility circle the user has to get the name of station to which he requires the visibility circle data file. The ground-trace data file and visibility circle data file are separately generated and these data files are used for graphical solution. The eccentric anomaly is chosen as the independent variable in order to avoid the iterative solution of Kepler's equation each time a ground point is desired. In this paper the analysis is developed about the adopted elements and their relation to the central planet about which the satellite moves; it is formulated for elliptic motion by using heliocentric-elliptic coordinate system, geocentric-equatorial coordinate system and perifocal coordinate system. Mercatro projection is employed to make world map on which ail spirals of constants compass heading appear as straight lines. Software consists of two-versions: a) the solution with Mercator projection and b) the solution without Mercator projection. The graphical solution provides a visual aid for comprehensive planning of certain critical operations. Ground station setting of this comes as a visual tool. It gives the graphical display about ground trace and visibility pattern over the selected ground station. It will be extensively used during planning phase of various missions, includes the geosynchronous transfer orbit and all types of low Earth orbits, and it is user friendly.
空间应用的图形解决方案
空间应用图形化解决方案旨在确定航天器的运行规划。该软件基本上给出了选定地面站的地面轨迹和可见性模式。宇宙飞船的地面轨迹是从给定的宇宙飞船上投下的光线的穿透点所形成的轨迹,其方向通常与运动发生的行星表面相交。在生成地迹时,要求用户给出生成地迹的卫星起始时间和关闭时间。要生成能见度圆的纬度和经度值,用户必须获得他需要能见度圆数据文件的站点名称。分别生成地迹数据文件和可见圈数据文件,用于图形化求解。选择偏心异常作为自变量是为了避免每次需要一个接地点时开普勒方程的迭代解。本文分析了卫星所采用的元素及其与卫星所绕中心行星的关系;采用日心-椭圆坐标系、地心-赤道坐标系和焦周坐标系对椭圆运动进行了公式化。用墨卡特罗投影法制作世界地图,在地图上,常数罗盘的所有螺旋都显示为直线。软件包括两个版本:a)有墨卡托投影的解决方案和b)没有墨卡托投影的解决方案。图形化解决方案为某些关键操作的全面规划提供了可视化辅助。地面站设置这是一个可视化的工具。给出了选定地面站的地面轨迹和能见度图的图形显示。它将在各种任务的规划阶段广泛使用,包括地球同步转移轨道和所有类型的近地轨道,它是用户友好的。
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