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
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