An Integrated System for Satellite Orbit Design and Mission Analysis

2004 ◽  
Author(s):  
Jinxiu Zhang ◽  
Xibin Cao
Keyword(s):  
Satellite Orbit ◽  
Integrated System ◽  
Orbit Design ◽  
Mission Analysis

scholarly journals Conceptual Satellite Orbit Design for Korean Navigation Satellite System

2018 ◽  
Vol 61 (1) ◽  
pp. 12-20 ◽  
Author(s):  
Moonseok CHOI ◽  
Dae Hee WON ◽  
Jongsun AHN ◽  
Sangkyoung SUNG ◽  
Jiyun LEE ◽  
...  
Keyword(s):  
Satellite Orbit ◽  
Satellite System ◽  
Navigation Satellite ◽  
Orbit Design

scholarly journals Preliminary Mission Analysis and Orbit Design for Next Mars Exploration

2010 ◽  
Vol 8 (ists27) ◽  
pp. Tk_7-Tk_12 ◽  
Author(s):  
Naoko OGAWA ◽  
Mutsuko Y. MORIMOTO ◽  
Yuichi TSUDA ◽  
Tetsuya YAMADA ◽  
Kazuhisa FUJITA ◽  
...  
Keyword(s):  
Orbit Design ◽  
Mars Exploration ◽  
Mission Analysis

scholarly journals OOST: An Object Oriented Tool for Satellite Orbit Design

2005 ◽  
Vol 2 (4) ◽  
pp. 806-818 ◽  
Author(s):  
Salem A.A ◽  
Zaki M. ◽  
Wahdan A.A
Keyword(s):  
Object Oriented ◽  
Satellite Orbit ◽  
Orbit Design

Optimal small satellite orbit design based on robust multi-objective optimization method

2017 ◽  
Vol 70 ◽  
pp. 339-350 ◽  
Author(s):  
Mingjun Pu ◽  
Jihe Wang ◽  
Dexin Zhang ◽  
Qingxian Jia ◽  
Xiaowei Shao
Keyword(s):  
Satellite Orbit ◽  
Optimization Method ◽  
Small Satellite ◽  
Multi Objective Optimization ◽  
Orbit Design ◽  
Multi Objective

Orbit Design and Simulation for Kufasat Nanosatellite

2015 ◽  
Vol 50 (4) ◽  
pp. 157-168 ◽  
Author(s):  
Mohammed Chessab Mahdi
Keyword(s):  
Low Earth Orbit ◽  
Earth Orbit ◽  
Analysis Tool ◽  
Solar Panels ◽  
Orbit Design ◽  
Polar Orbit ◽  
Mission Analysis ◽  
The Earth ◽  
General Mission Analysis Tool

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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