Zobrazeno 1 - 10
of 16
pro vyhledávání: '"William A. Maul"'
Autor:
Ann Patterson-Hine, Barton D. Baker, Amy K. Chicatelli, Eric Barszcz, William A. Maul, Gordon Aaseng, Kevin J. Melcher
Publikováno v:
Advances in Computational Intelligence and Autonomy for Aerospace Systems
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::14171362c3fe4f74f7aecc0ee9779b69
https://doi.org/10.2514/5.9781624104794.0047.0106
https://doi.org/10.2514/5.9781624104794.0047.0106
Publikováno v:
AIAA SPACE 2016.
A functional fault model (FFM) is an abstract representation of the failure space of a given system. As such, it simulates the propagation of failure effects along paths between the origin of the system failure modes and points within the system capa
Publikováno v:
AIAA Infotech @ Aerospace.
Functional fault models (FFMs) are qualitative representations of a system's failure space that are used to provide a diagnostic of the modeled system. An FFM simulates the failure effect propagation paths within a system between failure modes and ob
Publikováno v:
Journal of Aerospace Computing, Information, and Communication. 5:16-34
Aerospace systems are developed similarly to other large-scale systems through a series of reviews, where designs are modified as system requirements are refined. For space-based systems few are built and placed into service. These research vehicles
Autor:
Rachael A. Bis, William A. Maul
Publikováno v:
AIAA Infotech @ Aerospace.
Functional fault models (FFMs) are a directed graph representation of the failure effect propagation paths within a system's physical architecture and are used to support development and real-time diagnostics of complex systems. Verification of these
Publikováno v:
Infotech@Aerospace 2011.
This paper provides an overview of the analysis and reporting capabilities of the Extended Testability Analysis (ETA) Tool which is currently being prepared for release by researchers at the NASA Glenn Research Center. The ETA Tool is a software tool
Publikováno v:
AIAA Infotech@Aerospace 2010.
The NASA Ares I Crew Launch Vehicle is being designed to send astronauts into Earth orbit in support of missions to the International Space Station, to the moon, and beyond. The launch vehicle is an in-line two-stage rocket with the crew vehicle, Ori
Publikováno v:
AIAA SPACE 2007 Conference & Exposition.
The constraints of future Exploration Missions will require unique integrated system health management capabilities throughout the mission. An ambitious launch schedule, human-rating requirements, long quiescent periods, limited human access for repa
Autor:
Amy K. Chicatelli, Anupa Bajwa, Adam Sweet, Sandra C. Hayden, Christopher E. Fulton, Edward Balaban, William A. Maul
Publikováno v:
AIAA 1st Intelligent Systems Technical Conference.
The Propulsion IVHM Technology Experiment (PITEX) has been an on-going research effort conducted over several years. PITEX has developed and applied a model-based diagnostic system for the main propulsion system of the X-34 reusable launch vehicle, a
Publikováno v:
SAE Technical Paper Series.