DocumentCode :
2487672
Title :
Safing and fault protection for the MESSENGER mission to Mercury
Author :
Moore, Robert C.
Author_Institution :
Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
Volume :
2
fYear :
2002
fDate :
2002
Abstract :
The MErcury Surface, Space ENvironment, GEochemistry, and Ranging (MESSENGER) mission is a NASA Discovery-class, deep-space mission to orbit the planet Mercury. Its purpose is to map the planet surface using various scientific instruments and explore the interior of the planet using measurements from instruments such as a magnetometer and observation of planetary libration. This paper discusses the architecture and implementation of the methods by which faults in the MESSENGER spacecraft are detected and the effects of those faults mitigated. The responsibility of the redundant Fault Protection Processors (FPPs) is to detect faults and take autonomous corrective actions that will keep the spacecraft healthy and safe.
Keywords :
Mercury (planet); fault diagnosis; protection; space vehicles; MESSENGER deep-space mission; Mercury; fault detection; fault protection; magnetometer; planetary libration; redundant fault protection processor; safing architecture; scientific instrumentation; Extraterrestrial measurements; Fault detection; Instruments; Mercury (planets); NASA; Planetary orbits; Planets; Protection; Space missions; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 2002. Proceedings. The 21st
Print_ISBN :
0-7803-7367-7
Type :
conf
DOI :
10.1109/DASC.2002.1052952
Filename :
1052952
Link To Document :
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