This work presents the first part of the analysis, design and simulation of the reconfigurable control architecture for the Multi-Mission Platform (MMP), a generic service module currently under design at INPE. Its control system can be switched among nine main Modes of Operation. The implementation followed the specifications when they were found, otherwise it was designed. The manager block of the control system was implemented as a finite state machine. The tests were 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.
Analysis, Design and Simulation of the Transition from Pre-Nominal to Nominal Mode of the Reconfigurable Control Architecture for the Multi-Mission Platform
Sae Technical Papers
2008 SAE Brasil Congress and Exhibit ; 2008
2008-10-07
Conference paper
English
WIND Nominal Mission Performance and Extended Mission Design
British Library Conference Proceedings | 2001
|WIND Nominal Mission Performance and Extended Mission Design
Springer Verlag | 2001
|WIND Nominal Mission Performance and Extended Mission Design
Online Contents | 2001
|WIND Nominal Mission Performance and Extended Mission Design
Online Contents | 2001
|