TY - JOUR
T1 - SATLLA2.0
T2 - An Open Platform for Picosatellites
AU - Ronen, Rony
AU - Ben-Moshe, Boaz
N1 - Publisher Copyright:
IEEE
PY - 2023
Y1 - 2023
N2 - ”Space is hard” is a common expression among researchers and engineers who are trying to design, construct, test, and deploy satellites. This paper describes the design, development, and flight testing of a picosatellite for communication experiments and educational initiatives. The presented picosatellite,namedSATLLA-2B,weighs0.35kgandhasrecently completed a full operational year and a half in orbit. The picosatellite was fabricated using low-cost and commercially available components. It contains a high-resolution camera, an attitude determination and control system (ADCS), a payload board with edge-AI capabilities, and a LoRa-based communication framework that enables two-way communication when line of sight (LOS) is available. In addition, communication with the satellite is possible via other LoRa-based ground stations, eliminating the need to maintain a dedicated ground station. Flight test results demonstrated that the picosatellite successfully achieved its primary mission objectives. These included demonstrating LoRa RF technology for ad-hoc ground station communication (both uplink and downlink), relaying messages between two ground stations, and optimizing power management, among other accomplishments.
AB - ”Space is hard” is a common expression among researchers and engineers who are trying to design, construct, test, and deploy satellites. This paper describes the design, development, and flight testing of a picosatellite for communication experiments and educational initiatives. The presented picosatellite,namedSATLLA-2B,weighs0.35kgandhasrecently completed a full operational year and a half in orbit. The picosatellite was fabricated using low-cost and commercially available components. It contains a high-resolution camera, an attitude determination and control system (ADCS), a payload board with edge-AI capabilities, and a LoRa-based communication framework that enables two-way communication when line of sight (LOS) is available. In addition, communication with the satellite is possible via other LoRa-based ground stations, eliminating the need to maintain a dedicated ground station. Flight test results demonstrated that the picosatellite successfully achieved its primary mission objectives. These included demonstrating LoRa RF technology for ad-hoc ground station communication (both uplink and downlink), relaying messages between two ground stations, and optimizing power management, among other accomplishments.
KW - Dipole antennas
KW - LoRa Satellite Communication
KW - Open-Source for Nano-Satellite
KW - Payloads
KW - Picosatellite
KW - Satellite broadcasting
KW - Satellites
KW - Space vehicles
KW - Transceivers
KW - UHF antennas
UR - http://www.scopus.com/inward/record.url?scp=85179083149&partnerID=8YFLogxK
U2 - 10.1109/MAES.2023.3335336
DO - 10.1109/MAES.2023.3335336
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AN - SCOPUS:85179083149
SN - 0885-8985
SP - 1
EP - 10
JO - IEEE Aerospace and Electronic Systems Magazine
JF - IEEE Aerospace and Electronic Systems Magazine
ER -