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Experiences with the GPS in Unstabilized CubeSat
Published 2020-01-01“…The paper summarizes the experiences with the operation of the piNAV GPS receiver in a 1U unstabilized CubeSat operated on LEO orbit. piNAV L1 is a GPS receiver developed by an author for small satellite missions. …”
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Towards the Thousandth CubeSat: A Statistical Overview
Published 2019-01-01“…CubeSats have become an interesting innovation in the space sector. …”
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Electromechanical flight stabilization system for CubeSat nanosatellites
Published 2024-12-01“… The objective of the research was to design and simulate a stabilization system for attitude control of CubeSat nanosatellites in LEO orbit. The electronic system was inside the mechanical system, designed in Proteus. …”
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Design and manufacture of CubeSat-type nanosatellite thermal subsystem
Published 2025-01-01Subjects: “…CubeSat…”
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Design and Implementation of 3U CubeSat Platform Architecture
Published 2018-01-01“…This paper describes the main concept and development of a standard platform architecture of 3U Cube Satellite, whose design and performance were implemented and verified through the development of KAUSAT-5 3U CubeSat. The 3U standard platform is built in 1.5U size and developed as a modular concept to add and expand payloads and attitude control actuators to meet the user’s needs. …”
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High-Resolution Image and Video CubeSat (HiREV): Development of Space Technology Test Platform Using a Low-Cost CubeSat Platform
Published 2019-01-01“…Despite the emergence of the CubeSat technology worldwide, the CubeSat market in Korea is still in the beginning stages, and a standard testing platform is also in demand. …”
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Design, Analysis, Optimization, Manufacturing, and Testing of a 2U Cubesat
Published 2018-01-01“…The design optimization, development, and verification by analysis and testing of the 1st Greek cubesat, developed by the University of Patras and Libre Space Foundation (UPSat (University of Patras Satellite)), is presented. …”
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High-Accuracy and Low-Cost Attitude Measurement Unit of the CubeSat
Published 2020-01-01“…This paper proposes high-accuracy and reliable attitude measurement methods exclusive for CubeSat with restrictions of low cost, limited space, and low power consumption. …”
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A Low-Cost Photodiode Sun Sensor for CubeSat and Planetary Microrover
Published 2013-01-01“…This paper presents the development of low-cost methodologies to determine the attitude of a small, CubeSat-class satellite and a microrover relative to the sun's direction. …”
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Thermoelectric Generators Applied as a Power Source in CubeSats: State of the Art
Published 2025-01-01Subjects: Get full text
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Data Analysis and Results of the Radiation-Tolerant Collaborative Computer On-Board OPTOS CubeSat
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Physics‐Based Approach to Thermospheric Density Estimation Using CubeSat GPS Data
Published 2023-01-01Subjects: Get full text
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CubeSat’s Deployable Solar Panel with Viscoelastic Multilayered Stiffener for Launch Vibration Attenuation
Published 2020-01-01“…Ensuring the structural safety of a deployable solar panel under a severe launch vibration environment is one of the important factors for a successful CubeSat mission. A CubeSat’s deployable solar panel proposed in this study is effective to guarantee the structural safety of solar cells by attenuating launch loads owing to the superior damping characteristic achieved by a multilayered stiffener with viscoelastic acrylic tapes. …”
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An Architecture-Tracking Approach to Evaluate a Modular and Extensible Flight Software for CubeSat Nanosatellites
Published 2019-01-01Subjects: “…CubeSat…”
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On-Orbit Thermal Design and Validation of 1 U Standardized CubeSat of STEP Cube Lab
Published 2016-01-01“…The Cube Laboratory for Space Technology Experimental Projects (STEP Cube Lab) is a cube satellite (CubeSat) classified as a pico-class satellite of 1 U (unit) size. …”
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Achievements and Lessons Learned From Successful Small Satellite Missions for Space Weather‐Oriented Research
Published 2022-07-01Subjects: “…CubeSat…”
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Design of CubeSat-Based Multi-Regional Positioning Navigation and Timing System in Low Earth Orbit
Published 2024-12-01Subjects: Get full text
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Development of 6 U CubeSat’s Deployable Solar Panel with Burn Wire Triggering Holding and Release Mechanism
Published 2019-01-01“…In the present work, a deployable solar panel based on a burn wire triggering holding and release mechanism was developed for use of 6 U CubeSat. The holding and release mechanism was designed based on a nichrome burn wire cutting method widely used for CubeSat applications. …”
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Design of an Ultrawideband Circularly Polarized Printed Crossed-Dipole Antenna Based on Genetic Algorithms for S-Band CubeSat Applications
Published 2021-01-01“…As in any satellite, onboard antennas for CubeSats are crucial to establish communication with ground stations or other satellites. …”
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