Project
# | Title | Team Members | TA | Documents | Sponsor |
---|---|---|---|---|---|
33 | A 2D Model of Optical Satellite Communication System |
Jun Zheng Xuanyi Jin Yuxuan Li Zhijun Zhao |
design_document2.pdf proposal1.pdf |
Pavel Loskot | |
A 2D Model of Optical Satellite Communication System ##TEAM MEMBERS# Yuxuan Li (yuxuan43), Zhijun Zhao (zhijunz3), Xuanyi Jin (xuanyij2), Jun Zheng (junz6) ##PROBLEM## With the rapid development of aerospace and communication technologies, our demand for more multifunctional, stable, and advanced satellite communication products is increasing. Low Earth Orbit (LEO) satellites have gained widespread popularity due to their advantages, such as low latency and low deployment cost. They have shown promising potential in climate and geographical studies. With the advent of Starlink, LEO satellites have made their way into everyday households, delivering internet access to even the most remote areas. However, LEO satellites face a set of challenges. Since each satellite covers a smaller area and moves much faster than the Earth's rotation, a large constellation is required to ensure global coverage. Therefore, we believe that studying how these satellites communicate with ground stations is essential. We try to understand the dynamics of these interactions and optimize communication efficiency. ##SOLUTION OVERVIEW## We plan to design a 2D Model that simulates the movement of satellites along an orbit around the Earth. The basic of this model contains two disks and a few laser transmitters and receivers. There will be an inner disk that represents the earth and an outer disk that represents the satellite's orbit. Both the inner and outer disks will be rotating to represent the rotation of the Earth and the satellites’ rotation on the orbit around the Earth. There will be laser transmitters on the inner disk and receivers on the outer disk to represent satellites that receive optical signals. The receivers (satellites) can only receive the optical signal within a small scattering angle of the laser source. The rotation of the disks should be driven by motors under them, and there should be storage components for the satellite that preserve the signal for the following decoding process. The signal to be transferred should be converted to binary codes, 1 if the laser is emitted within a specific frequency and 0 if it is not emitted. To test the performance of this system in different situations, we need to develop a graphical user interface system that can control the rotation speed of each disk and the frequency of transmitting laser while demonstrating the impact on the efficiency of signal transmission by showing graphs. ##SOLUTION COMPONENT## Physical Simulation System: Orbits Simulation System: Two concentric disks, one representing Earth’s ground station, the other representing an orbiting LEO satellite. Motors with adjustable rotational speeds to mimic orbital characteristics. Signal Transmission Subsystem: A low-power laser that will be mounted on the Earth disk as the signal transmitter, The corresponding receiver(s) will be attached to the satellite disk as the signal receiver(s). Software Control and Monitoring System: A software application that can manage disk speeds and laser signal, capture the real-time data, and simulate the relative motion and signal transmission of ground-satellite communication. ##Criteria for Success## The 2D optical satellite communication model must remain stable under various conditions. Users should be able to adjust the satellite speed during the simulation through a graphical user interface (GUI). The satellite receiver should be able to detect the signal with sufficient strength. The system should decode the received signal into a readable message to demonstrate that once a signal is received, it can be used for practical purposes. The model should evaluate and display the efficiency of optical signal transmission. |