Telecommunication Subsystem Design of Satellite Constellation Based on Inter-Satellite-Link Idea

被引：0
|
作者：
Bohlouri, Vahid [1 ]
Joubary, Homeira Sheikhi [2 ]
Asadi, Mohammad Javad Torkaman [3 ]
Asadi, Mohammad Ali Torkaman [3 ]
机构：
[1] Montazeri Tech & Vocat Univ, Tech Fac, Mashhad, Razavi Khorasan, Iran
[2] Tarbiat Modares Univ, Dept Elect Engn, Tehran, Iran
[3] Sharif Univ Technol, Dept Aerosp Engn, Tehran, Iran
来源：
2020 28TH IRANIAN CONFERENCE ON ELECTRICAL ENGINEERING (ICEE) | 2020年
关键词：
CubeSat; Inter Satellite Link; Parabolic Radio Link Design; Reflector Antenna; Satellite Constellation;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
In this study, communication subsystem design of satellite constellation is performed based on inter-satellite-link idea. Three CubeSats are linked together as constellation form. To do this, orbit is intended in low earth and sun synchronous orbit in 600 Km altitude. Based on CubeSat design limitation and requirements, antenna is designed with deployable mechanism. S-band is considered for inter-satellitelink mission and X-band is selected for ground station data transfer. Link budget is calculated by considering losses for S & X-band. A high gain parabolic reflector antenna is designed and simulated as new idea. Finally, the simulation results show, satisfaction of requirements.
引用
收藏
页码：1016 / 1020
页数：5
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