Simulation System Optimization for Rotorcraft Research on the Vertical Motion Simulator

Simulation System Optimization for Rotorcraft Research on the Vertical Motion Simulator

A handling qualities experiment was run on the Vertical Motion Simulator using the GenHel math model configured for a UH60A Blackhawk helicopter. In order to obtain valid handling qualities ratings, the simulation system including the math model were optimized to provide realistic cues. The aircraft...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Beard, Steven D., Reardon, Scott, Tobias, Eric Luke, Aponso, Bimal Lalith
Format: Report
Sprache:eng
Schlagworte:
Aeronautics (General)
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator Beard, Steven D.
Reardon, Scott
Tobias, Eric Luke
Aponso, Bimal Lalith
description A handling qualities experiment was run on the Vertical Motion Simulator using the GenHel math model configured for a UH60A Blackhawk helicopter. In order to obtain valid handling qualities ratings, the simulation system including the math model were optimized to provide realistic cues. The aircraft math model was adjusted to account for the simulator motion system delays and the motion systems gains and washouts were tuned for the bob-up, precision hover and sidestep tasks. The handling qualities ratings from this experiment showed good correlation to flight ratings.
format Report
fullrecord <record><control><sourceid>nasa_CYI</sourceid><recordid>TN_cdi_nasa_ntrs_20120016838</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>20120016838</sourcerecordid><originalsourceid>FETCH-nasa_ntrs_201200168383</originalsourceid><addsrcrecordid>eNrjZAgPzswtzUksyczPUwiuLC5JzVXwLyjJzM2sgoil5RcpBOWX5BclFyWmlSgEpRanJhYlZygApUoyUhXCUotKMpMTcxR88yFGQEzLL-JhYE1LzClO5YXS3Awybq4hzh66eYnFifF5JUXF8UYGhkYGBoZmFsYWxgSkAT4QNkM</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Simulation System Optimization for Rotorcraft Research on the Vertical Motion Simulator</title><source>NASA Technical Reports Server</source><creator>Beard, Steven D. ; Reardon, Scott ; Tobias, Eric Luke ; Aponso, Bimal Lalith</creator><creatorcontrib>Beard, Steven D. ; Reardon, Scott ; Tobias, Eric Luke ; Aponso, Bimal Lalith</creatorcontrib><description>A handling qualities experiment was run on the Vertical Motion Simulator using the GenHel math model configured for a UH60A Blackhawk helicopter. In order to obtain valid handling qualities ratings, the simulation system including the math model were optimized to provide realistic cues. The aircraft math model was adjusted to account for the simulator motion system delays and the motion systems gains and washouts were tuned for the bob-up, precision hover and sidestep tasks. The handling qualities ratings from this experiment showed good correlation to flight ratings.</description><language>eng</language><publisher>Ames Research Center</publisher><subject>Aeronautics (General)</subject><creationdate>2012</creationdate><rights>Copyright Determination: PUBLIC_USE_PERMITTED</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>780,800,4490</link.rule.ids><linktorsrc>$$Uhttps://ntrs.nasa.gov/citations/20120016838$$EView_record_in_NASA$$FView_record_in_$$GNASA$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Beard, Steven D.</creatorcontrib><creatorcontrib>Reardon, Scott</creatorcontrib><creatorcontrib>Tobias, Eric Luke</creatorcontrib><creatorcontrib>Aponso, Bimal Lalith</creatorcontrib><title>Simulation System Optimization for Rotorcraft Research on the Vertical Motion Simulator</title><description>A handling qualities experiment was run on the Vertical Motion Simulator using the GenHel math model configured for a UH60A Blackhawk helicopter. In order to obtain valid handling qualities ratings, the simulation system including the math model were optimized to provide realistic cues. The aircraft math model was adjusted to account for the simulator motion system delays and the motion systems gains and washouts were tuned for the bob-up, precision hover and sidestep tasks. The handling qualities ratings from this experiment showed good correlation to flight ratings.</description><subject>Aeronautics (General)</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>2012</creationdate><recordtype>report</recordtype><sourceid>CYI</sourceid><recordid>eNrjZAgPzswtzUksyczPUwiuLC5JzVXwLyjJzM2sgoil5RcpBOWX5BclFyWmlSgEpRanJhYlZygApUoyUhXCUotKMpMTcxR88yFGQEzLL-JhYE1LzClO5YXS3Awybq4hzh66eYnFifF5JUXF8UYGhkYGBoZmFsYWxgSkAT4QNkM</recordid><startdate>20120813</startdate><enddate>20120813</enddate><creator>Beard, Steven D.</creator><creator>Reardon, Scott</creator><creator>Tobias, Eric Luke</creator><creator>Aponso, Bimal Lalith</creator><scope>CYE</scope><scope>CYI</scope></search><sort><creationdate>20120813</creationdate><title>Simulation System Optimization for Rotorcraft Research on the Vertical Motion Simulator</title><author>Beard, Steven D. ; Reardon, Scott ; Tobias, Eric Luke ; Aponso, Bimal Lalith</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-nasa_ntrs_201200168383</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>2012</creationdate><topic>Aeronautics (General)</topic><toplevel>online_resources</toplevel><creatorcontrib>Beard, Steven D.</creatorcontrib><creatorcontrib>Reardon, Scott</creatorcontrib><creatorcontrib>Tobias, Eric Luke</creatorcontrib><creatorcontrib>Aponso, Bimal Lalith</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Beard, Steven D.</au><au>Reardon, Scott</au><au>Tobias, Eric Luke</au><au>Aponso, Bimal Lalith</au><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Simulation System Optimization for Rotorcraft Research on the Vertical Motion Simulator</btitle><date>2012-08-13</date><risdate>2012</risdate><abstract>A handling qualities experiment was run on the Vertical Motion Simulator using the GenHel math model configured for a UH60A Blackhawk helicopter. In order to obtain valid handling qualities ratings, the simulation system including the math model were optimized to provide realistic cues. The aircraft math model was adjusted to account for the simulator motion system delays and the motion systems gains and washouts were tuned for the bob-up, precision hover and sidestep tasks. The handling qualities ratings from this experiment showed good correlation to flight ratings.</abstract><cop>Ames Research Center</cop><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_nasa_ntrs_20120016838
source NASA Technical Reports Server
subjects Aeronautics (General)
title Simulation System Optimization for Rotorcraft Research on the Vertical Motion Simulator
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-19T06%3A55%3A48IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-nasa_CYI&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=unknown&rft.btitle=Simulation%20System%20Optimization%20for%20Rotorcraft%20Research%20on%20the%20Vertical%20Motion%20Simulator&rft.au=Beard,%20Steven%20D.&rft.date=2012-08-13&rft_id=info:doi/&rft_dat=%3Cnasa_CYI%3E20120016838%3C/nasa_CYI%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true