View source for 18036899. COMMUNICATION SATELLITE SYSTEM, EARTH-SIDE CONTROL FACILITY, GROUND FACILITY, ARTIFICIAL SATELLITE, COMMUNICATION GROUND CENTER, AND TRANSMISSION ROUTE SEARCH DEVICE simplified abstract (Mitsubishi Electric Corporation)

=COMMUNICATION SATELLITE SYSTEM, EARTH-SIDE CONTROL FACILITY, GROUND FACILITY, ARTIFICIAL SATELLITE, COMMUNICATION GROUND CENTER, AND TRANSMISSION ROUTE SEARCH DEVICE=


==Organization Name==

[[:Category:Mitsubishi Electric Corporation|Mitsubishi Electric Corporation]]


[[Category:Mitsubishi Electric Corporation]]

==Inventor(s)==

[[:Category:Hisayuki Mukae of Tokyo (JP)|Hisayuki Mukae of Tokyo (JP)]][[Category:Hisayuki Mukae of Tokyo (JP)]]

==COMMUNICATION SATELLITE SYSTEM, EARTH-SIDE CONTROL FACILITY, GROUND FACILITY, ARTIFICIAL SATELLITE, COMMUNICATION GROUND CENTER, AND TRANSMISSION ROUTE SEARCH DEVICE - A simplified explanation of the abstract==


This abstract first appeared for US patent application 18036899 titled 'COMMUNICATION SATELLITE SYSTEM, EARTH-SIDE CONTROL FACILITY, GROUND FACILITY, ARTIFICIAL SATELLITE, COMMUNICATION GROUND CENTER, AND TRANSMISSION ROUTE SEARCH DEVICE

==Simplified Explanation==

The patent application describes a communication satellite system that includes communication satellites flying on different orbital planes. Each satellite has a fore-aft communication device to communicate with other satellites flying in front of and behind it. The satellites in each orbit form cross-link communication with satellites in adjacent orbits at the northern and southern edges of the orbit using the fore-aft communication device. This allows communication between orbits using only the fore-aft communication device.

* Communication satellite system with fore-aft communication devices
* Satellites fly on different orbital planes
* Satellites communicate with satellites in front and behind using fore-aft communication device
* Cross-link communication between satellites in adjacent orbits at the northern and southern edges
* Enables communication between orbits using only the fore-aft communication device

== Potential Applications ==
* Satellite communication systems
* Inter-satellite communication
* Global communication networks

== Problems Solved ==
* Facilitates communication between satellites in different orbits
* Reduces the need for complex communication systems
* Enables efficient and reliable communication in satellite systems

== Benefits ==
* Improved communication capabilities in satellite systems
* Simplified communication infrastructure
* Increased efficiency and reliability in inter-satellite communication


==Original Abstract Submitted==

In a communication satellite system (), communication satellites () that fly on respective orbital planes such as an orbit (A), an orbit (B), and an orbit (C) each include a fore-aft communication device for communicating with other communication satellites () flying in front of and behind that communication satellite (). Each of the communication satellites () flying in each orbit forms cross-link communication with communication satellites () in adjacent orbits at the northern edge of the orbit, indicated by a range (), and the southern edge of the orbit, indicated by a range (), using the fore-aft communication device. Thus, communication between orbits becomes possible only with the fore-aft communication device.



[[Category:H04B7/185]]
[[Category:H04B10/118]]
[[Category:H04B7/195]]