NASA LogoNTRSNTRS - NASA Technical Reports ServerSearchmore_vertCollectionsAboutNewsHelpLogin Back to ResultsSTOVL aircraft simulation for integrated flight and propulsion control researchThe United States is in the initial stages of committing to a national program to develop a supersonic short takeoff and vertical landing (STOVL) aircraft. The goal of the propulsion community in this effort is to have the enabling propulsion technologies for this type aircraft in place to permit a low risk decision regarding the initiation of a research STOVL supersonic attack/fighter aircraft in the late mid-90's. This technology will effectively integrate, enhance, and extend the supersonic cruise, STOVL and fighter/attack programs to enable U.S. industry to develop a revolutionary supersonic short takeoff and vertical landing fighter/attack aircraft in the post-ATF period. A joint NASA Lewis and NASA Ames research program, with the objective of developing and validating technology for integrated-flight propulsion control design methodologies for short takeoff and vertical landing (STOVL) aircraft, was planned and is underway. This program, the NASA Supersonic STOVL Integrated Flight-Propulsion Controls Program, is a major element of the overall NASA-Lewis Supersonic STOVL Propulsion Technology Program. It uses an integrated approach to develop an integrated program to achieve integrated flight-propulsion control technology. Essential elements of the integrated controls research program are realtime simulations of the integrated aircraft and propulsion systems which will be used in integrated control concept development and evaluations. This paper describes pertinent parts of the research program leading up to the related realtime simulation development and remarks on the simulation structure to accommodate propulsion system hardware drop-in for real system evaluation.Document ID19900004073Acquisition SourceLegacy CDMSDocument TypeConference PaperAuthorsMihaloew, James R.*(NASA Lewis Research Center Cleveland, OH, United States)*Drummond, Colin K.*(NASA Lewis Research Center Cleveland, OH, United States)*Date AcquiredSeptember 6, 2013Publication DateJanuary 1, 1989Subject CategoryAircraft Propulsion And PowerReport/Patent NumberNASA-TM-102419NAS 1.15:102419E-5185Meeting InformationMeeting: Applied Dynamics International Users Society Annual ConferenceLocation: Keystone, COCountry: United StatesStart Date: June 25, 1989End Date: June 28, 1989Accession Number90N13389Funding Number(s)PROJECT: RTOP 505-62-71Distribution LimitsPublicCopyrightWork of the US Gov. Public Use Permitted.Available DownloadsNameType19900004073.pdfSTIcloud_downloadcontent_copyvisibilityRelated RecordsThere are no records associated with this record.visibility_offNo Preview Available
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