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Software Validation of the JASON 1 Electrical Power Subsystem
Technical Paper
1999-01-2532
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
The aim of this paper is to describe the JASON 1 electrical power subsystem (EPS) and the associated validation method. JASON 1 EPS is based on an unregulated bus. On Board Software can connect and disconnect solar array sections to the satellite power bus according to instantaneous satellite needs. The EPS concept has been validated with simulation means based on the Saber® software. Saber® has a modeling language capable of reproducing the On-Board Software (OBS) battery management application as well as the behavior of the EPS equipment. A Tcl/Tk tool permitted to optimize the OBS parameters dedicated to the battery management and to check the EPS robustness.
Authors
Citation
Picart, G., Tastet, P., Ratsimandresy, A., Geneste, X. et al., "Software Validation of the JASON 1 Electrical Power Subsystem," SAE Technical Paper 1999-01-2532, 1999, https://doi.org/10.4271/1999-01-2532.Also In
References
- Low Earth Orbit Nickel Cadmium lifetime testing ESPC proceedings 1995 Hendel, B. Dudley G. 92-9092-318-0
- Tcl and the Tk Toolkit Outerhout John K. 0-201-63337-X