A Software for Establishing Technical Specifications of GEO Communication Satellites

Mehran Mirshams; Ehsan Zabihian

Volume 10, Issue 3 , December 2017, , Pages 1-14

Abstract
  This study introduces a new computer code termed AZMIN developed by Space Research Laboratory (SRL). This efficient tool which benefits from the Statistical Design Model (SDM) has been developed for the system design of GEO communication satellites. The main advantage of the AZMIN is to determine technical ...  Read More

Optimal Trajectory Design of an Upper Stage for Satellite Injection into Geostationary Orbit Using Limited Thrust

Mojtaba Alavi pour; Amir Ali Nikkhah; Jafar Roshanian

Volume 9, Issue 4 , April 2017, , Pages 13-25

Abstract
  In this research, the problem of optimal trajectory design of an upper stage is considered for satellite injection into Geostationary orbit in 3-Dimensional space. The optimal multi-burn trajectory is obtained based on Euler-Lagrange theory with minimum fuel consumption criteria. Instead of using switch ...  Read More

Analytical Solution to Relative Motion Dynamics in Satellite Formation Flying Using Geostationary Orbit Sets

Seyed Hossein Mortazavi

Volume 7, Issue 4 , January 2015, , Pages 11-21

Abstract
  Satellite formation flying is one of the most recent research topics in space field owing to various operational projects. The first and the most important step in facing with this concept is studying and modeling of dynamics of the problem. In this paper, the relative dynamics of a satellite formation ...  Read More