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タイトルIntegrated Tools for Future Distributed Engine Control Technologies
本文(外部サイト)http://hdl.handle.net/2060/20140001130
著者(英)Culley, Dennis; Saus, Joseph; Thomas, Randy
発行日2013-07-01
言語eng
内容記述Turbine engines are highly complex mechanical systems that are becoming increasingly dependent on control technologies to achieve system performance and safety metrics. However, the contribution of controls to these measurable system objectives is difficult to quantify due to a lack of tools capable of informing the decision makers. This shortcoming hinders technology insertion in the engine design process. NASA Glenn Research Center is developing a Hardware-inthe- Loop (HIL) platform and analysis tool set that will serve as a focal point for new control technologies, especially those related to the hardware development and integration of distributed engine control. The HIL platform is intended to enable rapid and detailed evaluation of new engine control applications, from conceptual design through hardware development, in order to quantify their impact on engine systems. This paper discusses the complex interactions of the control system, within the context of the larger engine system, and how new control technologies are changing that paradigm. The conceptual design of the new HIL platform is then described as a primary tool to address those interactions and how it will help feed the insertion of new technologies into future engine systems.
NASA分類Aircraft Propulsion and Power
レポートNONASA/TM-2013-217883
E-18694
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/83948


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