库法赛特纳米卫星轨道设计与仿真

IF 0.7 Q4 ASTRONOMY & ASTROPHYSICS

Artificial Satellites-Journal of Planetary Geodesy Pub Date : 2015-12-01 DOI:10.1515/arsa-2015-0013

M. Mahdi

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引用次数: 6

摘要

摘要介绍了库法特纳米卫星的轨道设计。极地轨道被选为KufaSat任务。轨道的倾角使卫星能够看到地球的每一个角落。KufaSat有一个用于成像目的的有效载荷，需要大量的能量，所以轨道被确定为与太阳同步，以便通过太阳能电池板提供能量。KufaSat任务是为低地球轨道设计的。计算了KufaSat的六个初始开普勒元素。首先利用MATLAB，然后利用通用任务分析工具对库法星根据开普勒元素计算的轨道设计进行了仿真分析。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Orbit Design and Simulation for Kufasat Nanosatellite

Abstract Orbit design for KufaSat Nano-satellites is presented. Polar orbit is selected for the KufaSat mission. The orbit was designed with an Inclination which enables the satellite to see every part of the earth. KufaSat has a payload for imaging purposes which require a large amount of power, so the orbit is determined to be sun synchronous in order to provide the power through solar panels. The KufaSat mission is designed for the low earth orbit. The six initial Keplerian Elements of KufaSat are calculated. The orbit design of KufaSat according to the calculated Keplerian elements has been simulated and analyzed by using MATLAB first and then by using General Mission Analysis Tool.

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来源期刊

Artificial Satellites-Journal of Planetary Geodesy ASTRONOMY & ASTROPHYSICS-

CiteScore

1.00

自引率

11.10%

发文量