Ali Ali

Ali Ali


Postgraduate Research Student

Academic and research departments

Institute for Communication Systems.

My publications

Publications

Ali Ali, Ahmed Massoud, Mazen O Hasna, Tamer Khattab, Taha Jabban, Mohammed Aref Nema (2019)Modeling of CubeSat Orientation Scenario and Solar Cells for Internet of Space Provision, In: 2019 9th International Conference on Recent Advances in Space Technologies (RAST)pp. 541-546 IEEE

As a cost-effective alternative to traditional satellites, CubeSats have emerged to provide new space experimentation opportunities. The power budgeting of CubeSats is an essential part of the designing process due to the size, weight, and available surface constraints, and hence the total generated power is affected by these constraints. Consequently, there is a considerable need for accurate determination of the received solar irradiation and the required energy storage. This paper presents a study pertinent to CubeSat power budgeting as an Internet of Space provider depending on determining the incident solar irradiation on its sides for Nadir-Orientation Scenario. The electrical power system should guarantee power provision during the CubeSat mission, which typically depends on solar cells conditions such as temperature and irradiation, along with the energy storage system.

Ali Ali, Mazen O Hasna (2019)Energy Harvesting Schemes for UAV based Communications, In: 2019 16th IEEE Annual Consumer Communications & Networking Conference (CCNC) IEEE

This paper presents two generic charging and transmission schemes to find the trade-off between the altitude of an Unmanned aerial vehicle (UAV) base station and the acquired harvested energy for maximum coverage area. The first scheme seeks the optimal balance between the coverage area and the harvested energy using simultaneous wireless charging and information transmission (SWCIT). The second scheme proposes time allocation to increase the UAV flying period where multiplexing information transmission and energy harvesting is optimized. Finally, the two schemes are implemented on a real UAV system to verify whether equipping it with energy harvesting technology is practical or not.

ALI ALI, MOHSEN KHALILY, ALI ARAGHI, RAHIM TAFAZOLLI (2021)Polarization-Insensitive Circular Reflectarray for Satellite Applications in Ka-band

A polarization-insensitive circular reflectarray antenna (RA) for long-distance wireless communications is investigated. By combining patches, dipoles, and rings, a polarization-insensitive unit cell is achieved. With a phase variation of around 314 • between 30 GHz and 32 GHz, a circular reflectarray with a radius of 400 mm is built. Simulation results indicate a maximum realized gain of 27.6 dB at 30 GHz.

ALI ALI, MOHSEN KHALILY, ALI ARAGHI, Seyed Ehsan Hosseininejad, RAHIM TAFAZOLLI (2021)A Circular Reflectarray for OAM Generation at Terahertz Regime for 6G Applications

A circular reflectarray antenna (RA) for generating Orbital Angular Momentum (OAM) modes in the Terahertz (THz) band is introduced. An interlaced unit cell is proposed to reach a phase variation of 328 at 185 GHz to 188 GHz. Combining RA, OAM, and THz technologies in one structure can be utilized to reach the future requirements of 6G networks. That is due to the additional degree of freedom that OAM beams can provide for data multiplexing in short-distance wireless communication.

Ali Jihad Ali, Mohsen Khalily, Ata Sattarzadeh, Ahmed Massoud, Mazen O Hasna, Tamer Khattab, Okan Yurduseven, Rahim Tafazolli (2021)Power Budgeting of LEO Satellites: An Electrical Power System Design for 5G Missions, In: IEEE Access9pp. 113258-113269 Institute of Electrical and Electronics Engineers (IEEE)

Although Geostationary-Equatorial-Orbit (GEO) satellites have achieved significant success in conducting space missions, they cannot meet the 5G latency requirements due to the far distance from the earth surface. Therefore, Low-Earth-Orbit (LEO) satellites arise as a potential solution for the latency problem. Nevertheless, integrating the 5G terrestrial networks with LEO satellites puts an increased burden on the satellites' limited budget, which stems from their miniature sizes, restricted weights, and the small available surface for solar harvesting in the presence of additional required equipment. This paper aims to design the Electrical Power System (EPS) for 5G LEO satellites and investigate altitudes that meet the latency and capacity requirements of 5G applications. In this regard, accurate solar irradiance determination for the nadir-orientation scenario, Multi-Junction (MJ) solar cells modeling, backup batteries type and number, and designing highly-efficient converters are addressed. Accordingly, the power budgeting of the 5G LEO satellite can be achieved based on defining the maximum generated power and determining the satellite's subsystem power requirements for 5G missions. In the sequel, the measured and simulated values of the electrical V-I characteristics of an MJ solar panel are compared to validate the model by using a Clyde Space solar panel that reaches a maximum power generation of approximately 1~W at ( I_{MPP}=0.426\,\,A , V_{MPP}=2.35\,\,V ). Moreover, a synchronous boost converter circuit is designed based on commercial off-the-shelf elements.