DocumentCode
3517050
Title
An Abort Failure Detection, Notification, & Response System: Overview of an ISHM Development Process
Author
Pisanich, Greg ; Bajwa, Anupa ; Sanderfer, Dwight ; Watson, Michael D.
Author_Institution
Perot Syst. Gov. Services, NASA Ames Res. Center, Moffett Field, CA
fYear
2008
fDate
1-8 March 2008
Firstpage
1
Lastpage
10
Abstract
Timely detection and response to catastrophic events during the launch and ascent phase of a launch system is of paramount importance to crew safety. This requires an abort system capable of detecting and confirming conditions that may lead to catastrophic failure, notifying the crew of the problem, and responding in time to allow the crew to escape safely. The development process for an Abort Failure Detection, Notification, and Response System is described. The process follows an iterative approach that first analyzes the vehicle design and identifies potential abort conditions. Those conditions are then characterized through modeling and simulation, with the results being used to identify required sensors and develop algorithms capable of detecting and responding to abort anomalies that could jeopardize the crew and mission. This process can be applied in the development of future crewed vehicles and other complex vehicle systems.
Keywords
alarm systems; fault diagnosis; space vehicles; abort failure detection notification and response system; ascent phase; crew safety; launch phase; launch system; vehicle design; Event detection; Fault detection; Intelligent sensors; Iterative algorithms; Moon; NASA; Phase detection; Propagation losses; Space vehicles; Vehicle detection;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2008 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-1487-1
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2008.4526643
Filename
4526643
Link To Document