TY - JOUR
T1 - The "intelligent valve"
T2 - A diagnostic framework for integrated system-health management of a rocket-engine test stand
AU - Russell, Michael J.
AU - Lecakes, George D.
AU - Mandayam, Shreekanth
AU - Jensen, Scott
N1 - Funding Information:
Manuscript received May 27, 2010; revised August 13, 2010; accepted October 5, 2010. Date of publication January 17, 2011; date of current version March 8, 2011. This work was supported in part by the National Aeronautics and Space Administration (NASA) Stennis Space Center under Grant/Cooperative Agreement—NNX08BA19A and in part by the NASA Graduate Student Researchers Program under Grants/Cooperative Agreements—NNX08AV98H and NNX07AO92H. The Associate Editor coordinating the review process for this paper was Dr. John Sheppard.
PY - 2011/4
Y1 - 2011/4
N2 - Valves play a critical role in rocket-engine test stands because they are essential for the cryogen transport mechanisms that are vital to test operations. Sensors that are placed on valves monitor the pressure, temperature, flow rate, valve position, and any other features that are required for diagnosing their functionality. Integrated system-health management (ISHM) algorithms have been used to identify and evaluate anomalous operating conditions of systems and subsystems (e.g., valves and valve components) on complex structures, such as rocket test stands. In order for such algorithms to be useful, there is a need to develop realistic models for the most common and problem-prone elements. Furthermore, the user needs to be provided with efficient tools to explore the nature of the anomaly and its possible effects on the element, as well as its relationship to the overall system state. This paper presents the development of an intelligent-valve framework that is capable of tracking and visualizing events of the large linear actuator valve (LLAV) in order to detect anomalous conditions. The framework employs a combination of technologies, including a dynamic data exchange data-transfer protocol, autoassociative neural networks, empirical and physical models, and virtual-reality environments. The diagnostic procedure that is developed has the ability to be integrated into existing ISHM systems and can be used for assessing the integrity of rocket-engine test-stand components.
AB - Valves play a critical role in rocket-engine test stands because they are essential for the cryogen transport mechanisms that are vital to test operations. Sensors that are placed on valves monitor the pressure, temperature, flow rate, valve position, and any other features that are required for diagnosing their functionality. Integrated system-health management (ISHM) algorithms have been used to identify and evaluate anomalous operating conditions of systems and subsystems (e.g., valves and valve components) on complex structures, such as rocket test stands. In order for such algorithms to be useful, there is a need to develop realistic models for the most common and problem-prone elements. Furthermore, the user needs to be provided with efficient tools to explore the nature of the anomaly and its possible effects on the element, as well as its relationship to the overall system state. This paper presents the development of an intelligent-valve framework that is capable of tracking and visualizing events of the large linear actuator valve (LLAV) in order to detect anomalous conditions. The framework employs a combination of technologies, including a dynamic data exchange data-transfer protocol, autoassociative neural networks, empirical and physical models, and virtual-reality environments. The diagnostic procedure that is developed has the ability to be integrated into existing ISHM systems and can be used for assessing the integrity of rocket-engine test-stand components.
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U2 - 10.1109/TIM.2010.2101350
DO - 10.1109/TIM.2010.2101350
M3 - Article
AN - SCOPUS:79952624973
SN - 0018-9456
VL - 60
SP - 1489
EP - 1497
JO - IEEE Transactions on Instrumentation and Measurement
JF - IEEE Transactions on Instrumentation and Measurement
IS - 4
M1 - 5688453
ER -