Application of Diagnostic Analysis Tools to the Ares I Thrust Vector Control System
Author:
Affiliation:
1. QinetiQ North America
2. NASA Marshall Space Flight Center
3. NASA Glenn Reseach Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-3451
Reference7 articles.
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2. 2Mohindra, S., and Clark, P. "A distributed fault diagnosis method based on digraph models: Steady-state analysis, computers andChemical Engineering," Volume17, issue 2,February 1993, pp.193-209.
3. Sensor Location Strategy in Large-Scale Systems for Fault Detection Applications
4. 4Zhang, Z., Wu, C., Zhang, B., Xia, T., and Li, A. "SDG Multiple Fault Diagnosis by Real-Time Inverse Inference, Reliability EngineeringandSystem Safety," Volume87, Issue2,February 2005,pp.173-189.
5. Multi-signal flow graphs: a novel approach for system testability analysis and fault diagnosis
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1. Advances in Functional Fault Modeling for the Design and Operation of Space Systems;Advances in Computational Intelligence and Autonomy for Aerospace Systems;2018-01
2. A Generic Modeling Process to Support Functional Fault Model Development;AIAA Infotech @ Aerospace;2016-01-01
3. Verification of Functional Fault Models and the Use of Resource Efficient Verification Tools;AIAA Infotech @ Aerospace;2015-01-02
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