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Analysis, Design and Simulation of the Reconfigurable Control Architecture for the Contingency mode of the Multimission Platform
Technical Paper
2010-36-0333
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
This work presents the analysis, design and simulation of the
reconfigurable control architecture for the contingency mode of the
MultiMission Platform (MMP). The MMP is a generic service module
currently under design at INPE. Its control system can be switched
among nine main Modes of Operation and other Sub-Modes, according
to ground command or information coming from the control system,
mainly alarms.
The implementation followed the specifications when they were
found, otherwise it was designed. They cover operations from
detumbling after launcher separation and solar acquisition, to
achieving payload nominal attitude and orbital corrections
maneuvers. The manager block of the control system was implemented
as a finite state machine.
The tests are based in simulations with the MatriX/SystemBuild
software. They focused mainly on the worst cases that the satellite
is supposed to endure in its mission, be it during modes or
transitions between modes and submodes. The tests show that the
model used satisfies the specifications.
Topic
Citation
Amaral, J. and de Oliveira e Souza, M., "Analysis, Design and Simulation of the Reconfigurable Control Architecture for the Contingency mode of the Multimission Platform," SAE Technical Paper 2010-36-0333, 2010, https://doi.org/10.4271/2010-36-0333.Also In
References
- AMARAL, J. C. Análise Projeto e Simulação de uma Arquitetura de Controle Reconfigurável para a Plataforma MultiMissão Dissertação (Mestrado em ETE/CMC) Instituto Nacional de Pesquisas Espaciais São José dos Campos, SP 2008
- BØGH, S. A. BLANKE, M. Fault-Tolerant Control A Case Study of the Ørsted Satellite Copenhagen, DEN 1997
- INPE MultiMission Platform Data Package for System Requirements Review (SRR) 2001 São José dos Campos, SP
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- SHIGEHARA, M. Geomagnetic Attitude Control of an Axisymmetric Spinning Satellite Journal of Spacecraft and Rockets 9 6 391 398 1972
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