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A Critical Embedded System Challenge: The FloripaSat-1 Mission
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A better irradiance estimation is useful for hardware-in-the-loop simulators that emulate orbit conditions or solar panels and batteries.
“A better irradiance estimation is useful for hardware in the loop simulators”
From Irradiation Flux Modelling for Thermal–Electrical Simulation of CubeSats: Orbit, Attitude and Radiation Integration (2020) · cites this paper as [23]
The case study uses the 1U CubeSat FloripaSat-I, whose orbit is nearly circular and Sun-synchronous with an altitude of 620 km.
“the case study is based on the CubeSat 1U FloripaSat-I, whose orbit is nearly-circular and Sun-synchronous, and has an altitude of 620 km [36].”
From An Integrated Thermal-Electrical Model for Simulations of Battery Behavior in CubeSats (2021) · cites this paper as [36]
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Metadata
- Authors
- Marcelino, G. M., Vega-Martinez, S., Seman, L. O., Kessler Slongo, L., & Bezerra, E. A.
- Affiliations
- Universidade Federal de Santa Catarina (BR)
- UFSC
- Universidade do Vale do Itajaí (BR)
- SENAI-SC
- Venue
- IEEE Latin America Transactions
- Published
- 2020-02
- Volume
- 18
- Issue
- 02
- Pages
- 249-256
- ISSN
- 1548-0992 (ISSN-L)
- OpenAlex
- W4255260926
- Cited by
- 34
- References
- 0
- Citations by year
- 2026: 1 · 2025: 7 · 2024: 4 · 2023: 7 · 2022: 5 · 2021: 6 · 2020: 4
- FWCI
- 3.30
- Type
- journal article
- Language
- en
- Open access
- closed
- Licence
- Locations
- IEEE Latin America Transactions (publishedVersion)
- Topics
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
- Physical Sciences › Engineering › Electrical and Electronic Engineering › Space Technology and Applications
- Physical Sciences › Engineering › Control and Systems Engineering › Embedded Systems and FPGA Design
- Keywords
- embedded systems, satellite missions, spacecraft software
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