Validation tests of attitude determination software for nanosatellite embedded systems

This article presents an assessment step of the development of a fault tolerant attitude determination system (SDATF) for nanosatellites. This system will be flight validated as payload of the NanosatC-BR2, a 2U-size cubesat that is being developed by the Brazilian Institute for Space Research (INPE...

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Veröffentlicht in:	Measurement : journal of the International Measurement Confederation 2018-02, Vol.116, p.391-401
Hauptverfasser:	Garcia, Camila B.A., Vale, Samuel R.C., Martins-Filho, Luiz S., Duarte, Ricardo O., Kuga, Helio K., Carrara, Valdemir
Format:	Artikel
Sprache:	eng
Schlagworte:	Algorithms Approximation Attitude control Attitude determination Computation Computer memory Computer simulation Control systems Cubesat Data processing Embedded systems Extraterrestrial radiation Fault tolerance Geomagnetic field model Geomagnetism Inertial coordinates Integrated circuits Mathematical models Missions Nanomaterials Nanosatellites Redundancy Satellites Software Solar position model Space research
Online-Zugang:	Volltext
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