A comprehensive attitude formulation with spin for numerical model of irradiance for CubeSats and Picosats
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For CubeSats, attitude becomes more critical because the available space for typical engineering solutions and the available external area for photovoltaic cells are very small.
“When dealing with small satellites as CubeSats, this becomes more critical as the available space to comport typical engineering solutions is very small, as the available external area for photovoltaic cells [13].”
From Irradiation Flux Modelling for Thermal–Electrical Simulation of CubeSats: Orbit, Attitude and Radiation Integration (2020) · cites this paper as [13]
The orbit, attitude, irradiance, and thermal models generalize the previous work presented in [17].
“The orbit and the following attitude, irradiance, and thermal models generalize the previous work presented in [17].”
From An Integrated Thermal-Electrical Model for Simulations of Battery Behavior in CubeSats (2021) · cites this paper as [17]
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“After that, the CubeSat’s normal vectors are rotated around the û⊥ by the angle Θ1 through the formulation of a rotation matrix around an arbitrary axis [13]:”
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- Authors
- Morsch Filho, E., Nicolau, V. D. P., Paiva, K. V. D., & Possamai, T. S.
- Affiliations
- Universidade Federal de Santa Catarina (BR)
- Venue
- Applied Thermal Engineering
- Publisher
- Elsevier BV
- Published
- 2020-03
- Volume
- 168
- Pages
- 114859
- ISSN
- 1359-4311 (ISSN-L)
- OpenAlex
- W2997791925
- Cited by
- 17
- References
- 37
- Citations by year
- 2026: 2 · 2025: 1 · 2024: 2 · 2023: 4 · 2022: 2 · 2021: 3 · 2020: 3
- FWCI
- 1.47
- Type
- journal article
- Language
- en
- Open access
- closed
- Locations
- Applied Thermal Engineering (publishedVersion)
- Funders
- CNPq
- National Council for Scientific and Technological Development
- Topics
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
- Physical Sciences › Engineering › Aerospace Engineering › Space Satellite Systems and Control
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Dynamics and Control
- Keywords
- CubeSat, spin motion, thermal irradiation, infrared radiation, eclipses, detumbling, orbital altitude
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