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タイトルFlight parameters monitoring system for tracking structural integrity of rotary-wing aircraft
本文(外部サイト)http://hdl.handle.net/2060/19950013053
著者(英)Mohammadi, Jamshid; Olkiewicz, Craig
著者所属(英)Systems and Electronics, Inc.
発行日1994-09-01
言語eng
内容記述Recent developments in advanced monitoring systems used in conjunction with tracking structural integrity of rotary-wing aircraft are explained. The paper describes: (1) an overview of rotary-wing aircraft flight parameters that are critical to the aircraft loading conditions and each parameter's specific requirements in terms of data collection and processing; (2) description of the monitoring system and its functions used in a survey of rotary-wing aircraft; and (3) description of the method of analysis used for the data. The paper presents a newly-developed method in compiling flight data. The method utilizes the maneuver sequence of events in several pre-identified flight conditions to describe various flight parameters at three specific weight ranges.
NASA分類AIRCRAFT DESIGN, TESTING AND PERFORMANCE
レポートNO95N19469
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/108749


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